Date:
February 11th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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 2087)
---------------------------------------
Vector Time (GMT): 2011/040/23:31:54
582
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2010534
04 A = 6733567
87 meter
Y = 5743631
43 meter E =
0003996
Z = -2876931
97 I = 51
99520
XDOT = -4152
189978 Wp = 352
85559
YDOT = 4004
197575 meter/sec RA = 92
38789 deg
ZDOT = 5095
529674 TA = 334
29576
MA = 334
31562
Ha = 191
496 n
mi
Hp = 188
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6596240
27 X = 1960133
64
Y = 18843935
15 feet Y = 5765832
57 meter
Z = -9438753
17 Z = -2867287
48
XDOT = -13622
670531 XDOT = -4221
409866
YDOT = 13137
131153 feet/sec YDOT = 3957
378358 meter/sec
ZDOT = 16717
617041 ZDOT = 5075
190417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9582735
32 X = 2920817
73
Y = -17535867
16 feet Y = -5344932
31 meter
Z = -9399940
73 Z = -2865101
94
XDOT = 17664
056112 XDOT = 5384
004303
YDOT = 741
023951 feet/sec YDOT = 225
864100 meter/sec
ZDOT = 16635
434495 ZDOT = 5070
480434
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 11040
98630018
00016717 00000-0 10270-3 0 9008
2 25544 51
6449 93
1777 0005020 292
4292 67
6338 15
72259759 20885
Satellite: ISS
Catalog Number: 25544
Epoch time: 11040
98630018 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 93
1777 deg
Eccentricity:
0005020
Arg of perigee: 292
4292 deg
Mean anomaly: 67
6338 deg
Mean motion: 15
72259759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2088
Checksum: 317
Coasting Arc #2 (Orbit 2103)
---------------------------------------
Vector Time (GMT): 2011/041/23:31:54
582
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3030166
09 A = 6729745
95 meter
Y = -4368738
07 meter E =
0005448
Z = -4131269
78 I = 51
98233
XDOT = 3245
929672 Wp = 28
92612
YDOT = 5847
441021 meter/sec RA = 87
33859 deg
ZDOT = -3800
176224 TA = 202
22677
MA = 202
25039
Ha = 191
512 n
mi
Hp = 188
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9941489
79 X = 3098861
60
Y = -14333130
13 feet Y = -4334468
85 meter
Z = -13554034
71 Z = -4116382
55
XDOT = 10649
375564 XDOT = 3198
761538
YDOT = 19184
517785 feet/sec YDOT = 5883
475206 meter/sec
ZDOT = -12467
769763 ZDOT = -3784
522345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17323001
15 X = -5280050
75
Y = 2411129
95 feet Y = 734912
41 meter
Z = -13493842
26 Z = -4112923
12
XDOT = 6934
389583 XDOT = 2113
601945
YDOT = -19649
585585 feet/sec YDOT = -5989
193686 meter/sec
ZDOT = -12404
709671 ZDOT = -3780
955508
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 11042
00324906
00016717 00000-0 10270-3 0 9010
2 25544 51
6446 87
9689 0005103 295
6343 64
4292 15
72278818 21049
Satellite: ISS
Catalog Number: 25544
Epoch time: 11042
00324906 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 87
9689 deg
Eccentricity:
0005103
Arg of perigee: 295
6343 deg
Mean anomaly: 64
4292 deg
Mean motion: 15
72278818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2104
Checksum: 303
Coasting Arc #3 (Orbit 2119)
---------------------------------------
Vector Time (GMT): 2011/042/23:31:54
582
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3539088
50 A = 6730890
12 meter
Y = -4340458
64 meter E =
0008290
Z = 3730757
36 I = 51
98480
XDOT = 2597
559546 Wp = 61
94550
YDOT = -5827
965085 meter/sec RA = 82
18928 deg
ZDOT = -4305
270972 TA = 73
33009
MA = 73
23910
Ha = 191
640 n
mi
Hp = 187
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11611182
74 X = -3508412
69
Y = -14240349
86 feet Y = -4379863
37 meter
Z = 12240017
57 Z = 3713639
22
XDOT = 8522
176989 XDOT = 2683
449792
YDOT = -19120
620358 feet/sec YDOT = -5798
437343 meter/sec
ZDOT = -14124
904763 ZDOT = -4292
443636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2167977
95 X = -660799
68
Y = 18291838
98 feet Y = 5575352
52 meter
Z = 12171017
10 Z = 3709726
01
XDOT = -18415
162931 XDOT = -5612
941661
YDOT = 7205
482979 feet/sec YDOT = 2196
231212 meter/sec
ZDOT = -14072
982857 ZDOT = -4289
445175
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 11043
02018056
00016717 00000-0 10270-3 0 9020
2 25544 51
6451 82
7599 0005119 301
4466 58
6196 15
72355335 21203
Satellite: ISS
Catalog Number: 25544
Epoch time: 11043
02018056 = yrday
fracday
Element set: 902
Inclination: 51
6451 deg
RA of node: 82
7599 deg
Eccentricity:
0005119
Arg of perigee: 301
4466 deg
Mean anomaly: 58
6196 deg
Mean motion: 15
72355335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2120
Checksum: 287
Coasting Arc #4 (Orbit 2135)
---------------------------------------
Vector Time (GMT): 2011/043/23:31:54
582
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1401689
11 A = 6732073
17 meter
Y = 5657425
47 meter E =
0008970
Z = 3358514
90 I = 51
98243
XDOT = -4662
227221 Wp = 69
90575
YDOT = -3944
220346 meter/sec RA = 77
14090 deg
ZDOT = 4691
215783 TA = 329
42030
MA = 329
47256
Ha = 191
862 n
mi
Hp = 187
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4598717
54 X = -1481162
08
Y = 18561107
17 feet Y = 5641306
52 meter
Z = 11018749
67 Z = 3351512
68
XDOT = -15296
021066 XDOT = -4640
564345
YDOT = -12940
355466 feet/sec YDOT = -3996
235141 meter/sec
ZDOT = 15391
127898 ZDOT = 4668
619665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16447771
64 X = 5013280
80
Y = -9785654
69 feet Y = -2982667
55 meter
Z = 10990337
43 Z = 3349854
85
XDOT = 967
312135 XDOT = 294
836739
YDOT = 18835
387736 feet/sec YDOT = 5741
026182 meter/sec
ZDOT = 15300
004534 ZDOT = 4663
441382
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 11044
03709725
00016717 00000-0 10270-3 0 9033
2 25544 51
6443 77
5501 0005114 305
2802 54
7881 15
72326050 21367
Satellite: ISS
Catalog Number: 25544
Epoch time: 11044
03709725 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 77
5501 deg
Eccentricity:
0005114
Arg of perigee: 305
2802 deg
Mean anomaly: 54
7881 deg
Mean motion: 15
72326050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2136
Checksum: 274
Coasting Arc #5 (Orbit 2150)
---------------------------------------
Vector Time (GMT): 2011/044/23:31:54
582
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4437344
48 A = 6728437
37 meter
Y = 2469216
46 meter E =
0004619
Z = -4418187
08 I = 51
96192
XDOT = -510
689859 Wp = 91
79747
YDOT = 6907
231422 meter/sec RA = 71
99172 deg
ZDOT = 3350
228434 TA = 211
75304
MA = 211
78090
Ha = 191
895 n
mi
Hp = 187
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14558216
79 X = 4430865
70
Y = 8101103
88 feet Y = 2518801
40 meter
Z = -14495364
44 Z = -4396646
64
XDOT = -1675
491664 XDOT = -604
164299
YDOT = 22661
520415 feet/sec YDOT = 6900
997866 meter/sec
ZDOT = 10991
563103 ZDOT = 3347
520660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4863286
89 X = -1482329
85
Y = -16013424
79 feet Y = -4880891
88 meter
Z = -14408463
40 Z = -4391699
64
XDOT = 15868
506180 XDOT = 4836
720684
YDOT = -14690
731444 feet/sec YDOT = -4477
734944 meter/sec
ZDOT = 10980
447638 ZDOT = 3346
840440
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 11044
99043905
00016717 00000-0 10270-3 0 9040
2 25544 51
6435 72
6658 0005077 307
7556 52
3146 15
72374774 21519
Satellite: ISS
Catalog Number: 25544
Epoch time: 11044
99043905 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 72
6658 deg
Eccentricity:
0005077
Arg of perigee: 307
7556 deg
Mean anomaly: 52
3146 deg
Mean motion: 15
72374774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2151
Checksum: 313
Coasting Arc #6 (Orbit 2166)
---------------------------------------
Vector Time (GMT): 2011/045/23:31:54
582
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -540490
84 A = 6734097
36 meter
Y = -6234676
68 meter E =
0000233
Z = -2486882
26 I = 51
96995
XDOT = 5265
021237 Wp = 122
31537
YDOT = 1678
541389 meter/sec RA = 66
93731 deg
ZDOT = -5352
911152 TA = 85
64351
MA = 85
64085
Ha = 191
927 n
mi
Hp = 187
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1773263
93 X = -458652
85
Y = -20454975
97 feet Y = -6240263
15 meter
Z = -8159062
54 Z = -2489309
21
XDOT = 17273
691722 XDOT = 5271
862916
YDOT = 5507
025554 feet/sec YDOT = 1737
456373 meter/sec
ZDOT = -17562
044461 ZDOT = -5327
317745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12737646
00 X = -3882434
50
Y = 16098001
86 feet Y = 4906670
97 meter
Z = -8168691
38 Z = -2489817
13
XDOT = -7732
796865 XDOT = -2356
956484
YDOT = -14977
006445 feet/sec YDOT = -4564
991565 meter/sec
ZDOT = -17458
754552 ZDOT = -5321
428387
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 11046
00732128
00016717 00000-0 10270-3 0 9057
2 25544 51
6429 67
4571 0005097 311
3872 48
6851 15
72380693 21677
Satellite: ISS
Catalog Number: 25544
Epoch time: 11046
00732128 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 67
4571 deg
Eccentricity:
0005097
Arg of perigee: 311
3872 deg
Mean anomaly: 48
6851 deg
Mean motion: 15
72380693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2167
Checksum: 308
Coasting Arc #7 (Orbit 2182)
---------------------------------------
Vector Time (GMT): 2011/046/23:31:54
582
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4592244
85 A = 6726387
56 meter
Y = -451230
64 meter E =
0007440
Z = 4894803
11 I = 51
93115
XDOT = -1769
534409 Wp = 16
32109
YDOT = -7126
420160 meter/sec RA = 61
79529 deg
ZDOT = -2309
283489 TA = 96
12153
MA = 96
03676
Ha = 192
082 n
mi
Hp = 187
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15066420
12 X = -4610635
11
Y = -1480415
50 feet Y = -502686
71 meter
Z = 16059065
32 Z = 4872450
03
XDOT = -5805
559086 XDOT = -1678
496192
YDOT = -23380
643570 feet/sec YDOT = -7145
699149 meter/sec
ZDOT = -7576
389399 ZDOT = -2317
658466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10240840
62 X = 3121408
22
Y = 11278482
03 feet Y = 3437681
32 meter
Z = 15968821
21 Z = 4867296
70
XDOT = -10610
801844 XDOT = -3234
172402
YDOT = 20445
900384 feet/sec YDOT = 6231
910437 meter/sec
ZDOT = -7610
008331 ZDOT = -2319
530539
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 11047
02418534
00016717 00000-0 10270-3 0 9063
2 25544 51
6429 62
2466 0005089 315
0145 45
0605 15
72421308 21833
Satellite: ISS
Catalog Number: 25544
Epoch time: 11047
02418534 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 62
2466 deg
Eccentricity:
0005089
Arg of perigee: 315
0145 deg
Mean anomaly: 45
0605 deg
Mean motion: 15
72421308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2183
Checksum: 280
Coasting Arc #8 (Orbit 2198)
---------------------------------------
Vector Time (GMT): 2011/047/23:31:54
582
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2527214
34 A = 6735541
16 meter
Y = 6042217
00 meter E =
0013752
Z = 1535914
13 I = 51
94562
XDOT = -5025
866384 Wp = 41
59711
YDOT = 621
953815 meter/sec RA = 56
72415 deg
ZDOT = 5803
498874 TA = 335
25803
MA = 335
32392
Ha = 192
070 n
mi
Hp = 187
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8291385
64 X = 2452000
36
Y = 19823546
57 feet Y = 6070057
34 meter
Z = 5039088
34 Z = 1548008
04
XDOT = -16489
062940 XDOT = -5060
639048
YDOT = 2040
530890 feet/sec YDOT = 565
557293 meter/sec
ZDOT = 19040
350635 ZDOT = 5778
999568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6842160
69 X = 2085490
58
Y = -20357113
76 feet Y = -6204848
27 meter
Z = 5087754
17 Z = 1550747
47
XDOT = 12351
978633 XDOT = 3764
883087
YDOT = 8901
264944 feet/sec YDOT = 2713
105555 meter/sec
ZDOT = 18941
408232 ZDOT = 5773
341229
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 11048
04103203
00016717 00000-0 10270-3 0 9071
2 25544 51
6416 57
0356 0004990 318
8435 41
2351 15
72454222 21996
Satellite: ISS
Catalog Number: 25544
Epoch time: 11048
04103203 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 57
0356 deg
Eccentricity:
0004990
Arg of perigee: 318
8435 deg
Mean anomaly: 41
2351 deg
Mean motion: 15
72454222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2199
Checksum: 281
Coasting Arc #9 (Orbit 2213)
---------------------------------------
Vector Time (GMT): 2011/048/23:31:54
582
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4023607
37 A = 6724945
23 meter
Y = -1478396
20 meter E =
0011271
Z = -5190931
49 I = 51
89157
XDOT = 3939
223597 Wp = 81
67867
YDOT = 6493
868879 meter/sec RA = 51
59430 deg
ZDOT = 1207
717325 TA = 199
81169
MA = 199
85550
Ha = 192
203 n
mi
Hp = 187
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13200811
58 X = 4065055
80
Y = -4850381
22 feet Y = -1433170
35 meter
Z = -17030615
12 Z = -5171284
69
XDOT = 12923
961933 XDOT = 3860
448478
YDOT = 21305
344091 feet/sec YDOT = 6537
479279 meter/sec
ZDOT = 3962
327183 ZDOT = 1226
661698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13290129
23 X = -4050831
39
Y = -4884394
19 feet Y = -1488763
35 meter
Z = -16951242
85 Z = -5166738
82
XDOT = 3549
109456 XDOT = 1081
768562
YDOT = -23629
336670 feet/sec YDOT = -7202
221817 meter/sec
ZDOT = 4038
641632 ZDOT = 1230
977969
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 11048
99431007
00016717 00000-0 10270-3 0 9082
2 25544 51
6408 52
1502 0004870 323
4872 36
5957 15
72476625 22148
Satellite: ISS
Catalog Number: 25544
Epoch time: 11048
99431007 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 52
1502 deg
Eccentricity:
0004870
Arg of perigee: 323
4872 deg
Mean anomaly: 36
5957 deg
Mean motion: 15
72476625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2214
Checksum: 304
Coasting Arc #10 (Orbit 2229)
---------------------------------------
Vector Time (GMT): 2011/049/23:31:54
582
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4273578
71 A = 6736182
42 meter
Y = -5170936
05 meter E =
0005936
Z = -585520
45 I = 51
91074
XDOT = 4005
320285 Wp = 131
80168
YDOT = -2633
462962 meter/sec RA = 46
50482 deg
ZDOT = -6019
647095 TA = 54
54118
MA = 54
48580
Ha = 192
248 n
mi
Hp = 186
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14020927
53 X = -4212594
44
Y = -16965013
29 feet Y = -5218384
86 meter
Z = -1920998
85 Z = -606132
31
XDOT = 13140
814584 XDOT = 4063
711985
YDOT = -8639
970348 feet/sec YDOT = -2588
347075 meter/sec
ZDOT = -19749
498343 ZDOT = -6000
047769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 122581
74 X = 37362
91
Y = 22001294
45 feet Y = 6705994
55 meter
Z = -2004080
25 Z = -610843
66
XDOT = -14130
642506 XDOT = -4307
019836
YDOT = -1700
768516 feet/sec YDOT = -518
394244 meter/sec
ZDOT = -19670
287171 ZDOT = -5995
503530
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 11050
01112076
00016717 00000-0 10270-3 0 9091
2 25544 51
6414 46
9403 0005049 328
4085 31
6773 15
72535245 22300
Satellite: ISS
Catalog Number: 25544
Epoch time: 11050
01112076 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 46
9403 deg
Eccentricity:
0005049
Arg of perigee: 328
4085 deg
Mean anomaly: 31
6773 deg
Mean motion: 15
72535245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2230
Checksum: 275
Coasting Arc #11 (Orbit 2245)
---------------------------------------
Vector Time (GMT): 2011/050/23:31:54
582
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2849396
12 A = 6724430
19 meter
Y = 3024588
68 meter E =
0004520
Z = 5286805
10 I = 51
84831
XDOT = -5711
917629 Wp = 1
79172
YDOT = -5161
040642 meter/sec RA = 41
38949 deg
ZDOT = -121
451193 TA = 89
38360
MA = 89
33181
Ha = 192
497 n
mi
Hp = 186
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9348412
48 X = -2908687
61
Y = 9923191
22 feet Y = 2992394
00 meter
Z = 17345161
08 Z = 5272818
76
XDOT = -18739
887233 XDOT = -5653
191400
YDOT = -16932
548037 feet/sec YDOT = -5224
586417 meter/sec
ZDOT = -398
461919 ZDOT = -149
055890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13566327
45 X = 4135016
61
Y = -1943215
67 feet Y = -592292
14 meter
Z = 17288603
91 Z = 5269566
47
XDOT = 4092
714837 XDOT = 1247
459482
YDOT = 23907
779401 feet/sec YDOT = 7287
091161 meter/sec
ZDOT = -509
771667 ZDOT = -155
378404
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 11051
02791602
00016717 00000-0 10270-3 0 9103
2 25544 51
6410 41
7290 0004751 332
2613 27
8296 15
72482892 22465
Satellite: ISS
Catalog Number: 25544
Epoch time: 11051
02791602 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 41
7290 deg
Eccentricity:
0004751
Arg of perigee: 332
2613 deg
Mean anomaly: 27
8296 deg
Mean motion: 15
72482892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2246
Checksum: 282
Coasting Arc #12 (Orbit 2260)
---------------------------------------
Vector Time (GMT): 2011/051/23:31:54
582
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5582311
92 A = 6736237
51 meter
Y = 3737097
95 meter E =
0014007
Z = -369843
34 I = 51
86573
XDOT = -2377
508922 Wp = 24
19083
YDOT = 4140
348993 meter/sec RA = 36
27765 deg
ZDOT = 6043
499125 TA = 331
80162
MA = 331
87740
Ha = 192
392 n
mi
Hp = 186
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18314671
66 X = 5541904
70
Y = 12260820
04 feet Y = 3799296
78 meter
Z = -1213396
80 Z = -342823
45
XDOT = -7800
226122 XDOT = -2452
988080
YDOT = 13583
822154 feet/sec YDOT = 4113
340766 meter/sec
ZDOT = 19827
753035 ZDOT = 6031
765691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7159634
22 X = -2182256
51
Y = -20850590
88 feet Y = -6355260
10 meter
Z = -1104416
38 Z = -336626
11
XDOT = 13006
289877 XDOT = 3964
317155
YDOT = -5496
113142 feet/sec YDOT = -1675
215286 meter/sec
ZDOT = 19780
258917 ZDOT = 6029
022918
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 11051
98114109
00016717 00000-0 10270-3 0 9110
2 25544 51
6417 36
8439 0004669 335
0038 25
0897 15
72557071 22618
Satellite: ISS
Catalog Number: 25544
Epoch time: 11051
98114109 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 36
8439 deg
Eccentricity:
0004669
Arg of perigee: 335
0038 deg
Mean anomaly: 25
0897 deg
Mean motion: 15
72557071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2261
Checksum: 302
Coasting Arc #13 (Orbit 2276)
---------------------------------------
Vector Time (GMT): 2011/052/23:31:54
582
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1236950
22 A = 6724366
02 meter
Y = -4059706
95 meter E =
0014362
Z = -5227852
09 I = 51
80152
XDOT = 6879
398909 Wp = 64
58578
YDOT = 3303
900938 meter/sec RA = 31
17876 deg
ZDOT = -933
891941 TA = 196
49950
MA = 196
54629
Ha = 192
432 n
mi
Hp = 186
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4058235
63 X = 1307650
29
Y = -13319248
52 feet Y = -4045479
70 meter
Z = -17151745
70 Z = -5221671
05
XDOT = 22570
206393 XDOT = 6846
479383
YDOT = 10839
570005 feet/sec YDOT = 3380
646409 meter/sec
ZDOT = -3063
949937 ZDOT = -900
552512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11234810
94 X = -3424370
37
Y = 8277096
38 feet Y = 2522858
98 meter
Z = -17126667
42 Z = -5220208
23
XDOT = -11194
262900 XDOT = -3412
011332
YDOT = -21283
405275 feet/sec YDOT = -6487
181928 meter/sec
ZDOT = -2929
451912 ZDOT = -892
896943
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 11052
99789769
00016717 00000-0 10270-3 0 9123
2 25544 51
6424 31
6343 0004574 340
8420 19
2570 15
72598521 22772
Satellite: ISS
Catalog Number: 25544
Epoch time: 11052
99789769 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 31
6343 deg
Eccentricity:
0004574
Arg of perigee: 340
8420 deg
Mean anomaly: 19
2570 deg
Mean motion: 15
72598521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2277
Checksum: 319
Coasting Arc #14 (Orbit 2292)
---------------------------------------
Vector Time (GMT): 2011/053/23:31:54
582
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6308497
17 A = 6735417
31 meter
Y = -1993129
06 meter E =
0010746
Z = 1244938
58 I = 51
81192
XDOT = 396
893121 Wp = 104
67843
YDOT = -4952
521327 meter/sec RA = 26
04553 deg
ZDOT = -5878
368659 TA = 61
71327
MA = 61
60487
Ha = 192
453 n
mi
Hp = 186
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20697169
19 X = -6291788
37
Y = -6539137
35 feet Y = -2063581
01 meter
Z = 4084444
16 Z = 1214333
00
XDOT = 1302
142786 XDOT = 480
799328
YDOT = -16248
429550 feet/sec YDOT = -4947
614178 meter/sec
ZDOT = -19285
986415 ZDOT = -5876
236524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13136662
43 X = 4004054
71
Y = 17307651
32 feet Y = 5275372
12 meter
Z = 3960949
36 Z = 1207297
36
XDOT = -9281
581100 XDOT = -2829
025919
YDOT = 11486
977523 feet/sec YDOT = 3501
230749 meter/sec
ZDOT = -19277
220834 ZDOT = -5875
696910
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 11054
01463318
00016717 00000-0 10270-3 0 9138
2 25544 51
6420 26
4229 0004743 342
6428 17
4572 15
72639962 22934
Satellite: ISS
Catalog Number: 25544
Epoch time: 11054
01463318 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 26
4229 deg
Eccentricity:
0004743
Arg of perigee: 342
6428 deg
Mean anomaly: 17
4572 deg
Mean motion: 15
72639962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2293
Checksum: 296
Coasting Arc #15 (Orbit 2308)
---------------------------------------
Vector Time (GMT): 2011/054/23:31:54
582
Vector Time (MET): N/A
Weight (LBS) : 863480
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 571226
10 A = 6725076
42 meter
Y = 4447193
29 meter E =
0003753
Z = 5008882
31 I = 51
75003
XDOT = -7362
540426 Wp = 69
63830
YDOT = -1206
636482 meter/sec RA = 20
95752 deg
ZDOT = 1911
100885 TA = 1
94264
MA = 1
94118
Ha = 192
515 n
mi
Hp = 186
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1874101
38 X = 497122
39
Y = 14590529
17 feet Y = 4453166
90 meter
Z = 16433340
92 Z = 5011477
16
XDOT = -24155
316357 XDOT = -7357
784036
YDOT = -3958
781108 feet/sec YDOT = -1288
942212 meter/sec
ZDOT = 6270
016028 ZDOT = 1875
345772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6755804
10 X = 2059169
09
Y = -13054322
57 feet Y = -3978957
52 meter
Z = 16443669
43 Z = 5012030
44
XDOT = 16802
157229 XDOT = 5121
297523
YDOT = 16410
973922 feet/sec YDOT = 5002
064852 meter/sec
ZDOT = 6125
710129 ZDOT = 1867
116447
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 11055
03135112
00016717 00000-0 10270-3 0 9140
2 25544 51
6426 21
2123 0004595 346
8854 13
2188 15
72656624 23099
Satellite: ISS
Catalog Number: 25544
Epoch time: 11055
03135112 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 21
2123 deg
Eccentricity:
0004595
Arg of perigee: 346
8854 deg
Mean anomaly: 13
2188 deg
Mean motion: 15
72656624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2309
Checksum: 283
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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