Date:
July 29th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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
213/08:19:49
531 2
0 3
3 3
3
N/A 1
7 0
0 189
2
000/00:05:39
061 -1
9 0
0 187
2
Coasting Arc #1 (Orbit 1227)
---------------------------------------
Vector Time (GMT): 2009/208/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3359922
62 A = 6721478
27 meter
Y = -3115251
58 meter E =
0005393
Z = 4919953
79 I = 51
95228
XDOT = 2968
428083 Wp = 355
41244
YDOT = -6742
333676 meter/sec RA = 100
01516 deg
ZDOT = -2236
878023 TA = 116
26576
MA = 116
21033
Ha = 188
406 n
mi
Hp = 185
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11023368
19 X = -3348737
68
Y = -10220641
68 feet Y = -3152762
00 meter
Z = 16141580
68 Z = 4903658
38
XDOT = 9738
937281 XDOT = 3054
467648
YDOT = -22120
517311 feet/sec YDOT = -6708
657749 meter/sec
ZDOT = -7338
838657 ZDOT = -2222
248988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14636109
18 X = -4461086
08
Y = 3718881
27 feet Y = 1133515
01 meter
Z = 16077344
92 Z = 4900374
73
XDOT = -12900
332907 XDOT = -3932
021470
YDOT = -19218
453465 feet/sec YDOT = -5857
784616 meter/sec
ZDOT = -7281
675007 ZDOT = -2219
454542
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 09208
35632049
00010596 00000-0 82463-4 0 9001
2 25544 51
6389 100
6175 0006191 287
8925 72
1563 15
74088899 12288
Satellite: ISS
Catalog Number: 25544
Epoch time: 09208
35632049 = yrday
fracday
Element set: 900
Inclination: 51
6389 deg
RA of node: 100
6175 deg
Eccentricity:
0006191
Arg of perigee: 287
8925 deg
Mean anomaly: 72
1563 deg
Mean motion: 15
74088899 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1228
Checksum: 329
Coasting Arc #2 (Orbit 1243)
---------------------------------------
Vector Time (GMT): 2009/209/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2092495
75 A = 6730098
98 meter
Y = 6069056
72 meter E =
0010434
Z = 1998710
20 I = 51
98598
XDOT = -4126
037971 Wp = 44
49627
YDOT = -3276
662750 meter/sec RA = 94
93770 deg
ZDOT = 5619
635949 TA = 337
67091
MA = 337
71630
Ha = 188
529 n
mi
Hp = 185
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6865143
55 X = -2169914
78
Y = 19911603
41 feet Y = 6045224
17 meter
Z = 6557448
16 Z = 1988357
35
XDOT = -13536
869985 XDOT = -4116
390130
YDOT = -10750
205874 feet/sec YDOT = -3322
749033 meter/sec
ZDOT = 18437
125817 ZDOT = 5599
614940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13180856
19 X = 4017524
97
Y = 16443702
14 feet Y = 5012040
41 meter
Z = 6517051
72 Z = 1986397
36
XDOT = -15164
284701 XDOT = -4622
073977
YDOT = 4866
051677 feet/sec YDOT = 1483
172551 meter/sec
ZDOT = 18358
235151 ZDOT = 5595
590074
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 09209
37208560
00010596 00000-0 82463-4 0 9012
2 25544 51
6392 95
4000 0006204 291
1447 68
9053 15
74127956 12445
Satellite: ISS
Catalog Number: 25544
Epoch time: 09209
37208560 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 95
4000 deg
Eccentricity:
0006204
Arg of perigee: 291
1447 deg
Mean anomaly: 68
9053 deg
Mean motion: 15
74127956 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1244
Checksum: 297
Coasting Arc #3 (Orbit 1258)
---------------------------------------
Vector Time (GMT): 2009/210/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3830733
49 A = 6721559
14 meter
Y = 2589984
08 meter E =
0006045
Z = -4883600
51 I = 51
95892
XDOT = -1810
810755 Wp = 97
61532
YDOT = 7102
193924 meter/sec RA = 89
78810 deg
ZDOT = 2347
863259 TA = 195
16532
MA = 195
18345
Ha = 188
817 n
mi
Hp = 185
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12568023
28 X = 3825210
67
Y = 8497323
11 feet Y = 2632791
18 meter
Z = -16022311
37 Z = -4865004
06
XDOT = -5940
980166 XDOT = -1901
499557
YDOT = 23301
161167 feet/sec YDOT = 7081
437084 meter/sec
ZDOT = 7702
963449 ZDOT = 2338
846781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13824441
47 X = 4213689
76
Y = -6433236
11 feet Y = -1960850
36 meter
Z = -15949058
35 Z = -4861272
99
XDOT = 16367
605473 XDOT = 4988
846148
YDOT = 16176
306158 feet/sec YDOT = 4930
538117 meter/sec
ZDOT = 7667
861319 ZDOT = 2337
164130
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 09210
32435685
00010596 00000-0 82463-4 0 9020
2 25544 51
6397 90
5087 0006313 295
9313 64
1199 15
74120609 12599
Satellite: ISS
Catalog Number: 25544
Epoch time: 09210
32435685 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 90
5087 deg
Eccentricity:
0006313
Arg of perigee: 295
9313 deg
Mean anomaly: 64
1199 deg
Mean motion: 15
74120609 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1259
Checksum: 309
Coasting Arc #4 (Orbit 1274)
---------------------------------------
Vector Time (GMT): 2009/211/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1076950
03 A = 6729817
84 meter
Y = -6296235
60 meter E =
0002083
Z = -2114183
70 I = 51
98660
XDOT = 4611
548073 Wp = 217
96426
YDOT = 2656
643503 meter/sec RA = 84
71258 deg
ZDOT = -5561
367632 TA = 345
54001
MA = 345
54597
Ha = 188
883 n
mi
Hp = 185
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3533300
62 X = 1157545
83
Y = -20656940
95 feet Y = -6283741
64 meter
Z = -6936298
23 Z = -2108756
84
XDOT = 15129
750895 XDOT = 4608
514253
YDOT = 8716
021992 feet/sec YDOT = 2708
196191 meter/sec
ZDOT = -18245
956799 ZDOT = -5538
971930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16057406
83 X = -4894297
60
Y = -13477556
20 feet Y = -4107959
13 meter
Z = -6915259
97 Z = -2107771
24
XDOT = 14212
752406 XDOT = 4332
046933
YDOT = -7614
534537 feet/sec YDOT = -2320
910127 meter/sec
ZDOT = -18157
760568 ZDOT = -5534
485421
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 09211
34010154
00010596 00000-0 82463-4 0 9034
2 25544 51
6406 85
2915 0006360 300
2677 59
7856 15
74149125 12758
Satellite: ISS
Catalog Number: 25544
Epoch time: 09211
34010154 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 85
2915 deg
Eccentricity:
0006360
Arg of perigee: 300
2677 deg
Mean anomaly: 59
7856 deg
Mean motion: 15
74149125 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1275
Checksum: 292
Coasting Arc #5 (Orbit 1290)
---------------------------------------
Vector Time (GMT): 2009/212/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4215010
67 A = 6721705
72 meter
Y = -2036188
20 meter E =
0007227
Z = 4825784
98 I = 51
95561
XDOT = 645
149458 Wp = 7
11408
YDOT = -7256
360141 meter/sec RA = 79
56161 deg
ZDOT = -2490
839450 TA = 107
18115
MA = 107
10202
Ha = 189
103 n
mi
Hp = 185
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13828775
17 X = -4215371
00
Y = -6680407
50 feet Y = -2083325
53 meter
Z = 15832627
88 Z = 4805307
49
XDOT = 2116
632080 XDOT = 738
343317
YDOT = -23806
955842 feet/sec YDOT = -7248
624321 meter/sec
ZDOT = -8172
045441 ZDOT = -2487
479865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12623732
68 X = -3847713
72
Y = 8891049
25 feet Y = 2709991
81 meter
Z = 15752002
70 Z = 4801210
42
XDOT = -19075
828729 XDOT = -5814
312597
YDOT = -12585
701260 feet/sec YDOT = -3836
121744 meter/sec
ZDOT = -8159
171424 ZDOT = -2486
915450
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 09212
35583565
00010596 00000-0 82463-4 0 9048
2 25544 51
6409 80
0747 0006368 304
1255 55
9304 15
74156124 12911
Satellite: ISS
Catalog Number: 25544
Epoch time: 09212
35583565 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 80
0747 deg
Eccentricity:
0006368
Arg of perigee: 304
1255 deg
Mean anomaly: 55
9304 deg
Mean motion: 15
74156124 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1291
Checksum: 299
Coasting Arc #6 (Orbit 1306)
---------------------------------------
Vector Time (GMT): 2009/213/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -57319
35 A = 6729513
12 meter
Y = 6338137
15 meter E =
0011743
Z = 2238490
53 I = 51
97557
XDOT = -5015
585398 Wp = 44
47390
YDOT = -1990
825359 meter/sec RA = 74
48674 deg
ZDOT = 5499
414715 TA = 340
53331
MA = 340
57812
Ha = 189
260 n
mi
Hp = 185
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -188055
62 X = -139063
28
Y = 20794413
23 feet Y = 6337038
83 meter
Z = 7344129
05 Z = 2238014
34
XDOT = -16455
332672 XDOT = -5019
665733
YDOT = -6531
579262 feet/sec YDOT = -2046
936094 meter/sec
ZDOT = 18042
699197 ZDOT = 5475
039111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18213409
16 X = 5551447
11
Y = 10036831
72 feet Y = 3059226
31 meter
Z = 7342544
11 Z = 2238007
44
XDOT = -12853
989189 XDOT = -3917
895905
YDOT = 10174
753410 feet/sec YDOT = 3101
264839 meter/sec
ZDOT = 17946
742391 ZDOT = 5470
167081
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 09213
37155849
00010596 00000-0 82463-4 0 9052
2 25544 51
6410 74
8569 0006447 308
3071 51
7512 15
74171157 13072
Satellite: ISS
Catalog Number: 25544
Epoch time: 09213
37155849 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 74
8569 deg
Eccentricity:
0006447
Arg of perigee: 308
3071 deg
Mean anomaly: 51
7512 deg
Mean motion: 15
74171157 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1307
Checksum: 304
Coasting Arc #7 (Orbit 1306)
---------------------------------------
Vector Time (GMT): 2009/213/08:22:39
061
Vector Time (MET): N/A
Weight (LBS) : 672427
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2049134
61 A = 6725782
45 meter
Y = -4844028
91 meter E =
0004898
Z = -4195863
52 I = 51
95816
XDOT = 4435
904124 Wp = 9
90597
YDOT = 5084
827017 meter/sec RA = 74
30525 deg
ZDOT = -3699
872942 TA = 222
45183
MA = 222
48972
Ha = 189
179 n
mi
Hp = 187
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6722882
59 X = 2123531
58
Y = -15892483
30 feet Y = -4820697
77 meter
Z = -13765956
43 Z = -4185728
85
XDOT = 14553
491219 XDOT = 4396
688136
YDOT = 16682
503336 feet/sec YDOT = 5134
213103 meter/sec
ZDOT = -12138
690754 ZDOT = -3678
418168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13586171
28 X = -4141065
01
Y = -10689896
31 feet Y = -3258280
39 meter
Z = -13726317
75 Z = -4183781
65
XDOT = 19123
227803 XDOT = 5828
759834
YDOT = -8809
159502 feet/sec YDOT = -2685
031816 meter/sec
ZDOT = -12054
080708 ZDOT = -3674
083800
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 09213
37156423
00010596 00000-0 82463-4 0 9062
2 25544 51
6421 74
8575 0007036 286
9954 73
0438 15
73575209 13076
Satellite: ISS
Catalog Number: 25544
Epoch time: 09213
37156423 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 74
8575 deg
Eccentricity:
0007036
Arg of perigee: 286
9954 deg
Mean anomaly: 73
0438 deg
Mean motion: 15
73575209 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1307
Checksum: 318
Coasting Arc #8 (Orbit 1322)
---------------------------------------
Vector Time (GMT): 2009/214/08:22:39
061
Vector Time (MET): N/A
Weight (LBS) : 672427
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4297864
47 A = 6728670
06 meter
Y = -3961107
22 meter E =
0006466
Z = 3330702
93 I = 51
95798
XDOT = 1721
738655 Wp = 70
37502
YDOT = -5838
743500 meter/sec RA = 69
14555 deg
ZDOT = -4712
667620 TA = 70
67356
MA = 70
60365
Ha = 189
402 n
mi
Hp = 187
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14100605
21 X = -4269430
97
Y = -12995758
60 feet Y = -4009009
90 meter
Z = 10927503
05 Z = 3309892
79
XDOT = 5648
748868 XDOT = 1809
793455
YDOT = -19155
982610 feet/sec YDOT = -5818
997075 meter/sec
ZDOT = -15461
507938 ZDOT = -4704
090394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16043047
09 X = -4889920
75
Y = 10588833
19 feet Y = 3227476
36 meter
Z = 10845477
57 Z = 3305701
56
XDOT = -16420
101060 XDOT = -5004
846803
YDOT = -9043
867088 feet/sec YDOT = -2756
570688 meter/sec
ZDOT = -15428
032604 ZDOT = -4702
464338
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 09214
38767730
00010596 00000-0 82463-4 0 9074
2 25544 51
6417 69
6430 0007058 290
5559 69
4846 15
73563841 13238
Satellite: ISS
Catalog Number: 25544
Epoch time: 09214
38767730 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 69
6430 deg
Eccentricity:
0007058
Arg of perigee: 290
5559 deg
Mean anomaly: 69
4846 deg
Mean motion: 15
73563841 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1323
Checksum: 332
Coasting Arc #9 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2009/215/08:22:39
061
Vector Time (MET): N/A
Weight (LBS) : 672427
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -941823
46 A = 6726293
75 meter
Y = 5294158
31 meter E =
0004115
Z = 4036824
58 I = 51
93893
XDOT = -5328
680918 Wp = 80
63232
YDOT = -3940
405109 meter/sec RA = 64
08517 deg
ZDOT = 3921
770479 TA = 329
05392
MA = 329
07816
Ha = 189
692 n
mi
Hp = 186
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3089971
97 X = -1020563
44
Y = 17369285
80 feet Y = 5283185
56 meter
Z = 13244175
13 Z = 4032058
65
XDOT = -17482
548942 XDOT = -5303
273492
YDOT = -12927
838285 feet/sec YDOT = -3999
851939 meter/sec
ZDOT = 12866
701048 ZDOT = 3895
945479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16205578
22 X = 4939460
24
Y = 7007801
83 feet Y = 2135978
00 meter
Z = 13225662
14 Z = 4031181
82
XDOT = -16047
608881 XDOT = -4891
311187
YDOT = 13002
363987 feet/sec YDOT = 3963
120543 meter/sec
ZDOT = 12764
948877 ZDOT = 3890
756418
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 09215
40377915
00010596 00000-0 82463-4 0 9081
2 25544 51
6421 64
4276 0007115 295
1104 64
9320 15
73583766 13397
Satellite: ISS
Catalog Number: 25544
Epoch time: 09215
40377915 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 64
4276 deg
Eccentricity:
0007115
Arg of perigee: 295
1104 deg
Mean anomaly: 64
9320 deg
Mean motion: 15
73583766 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1339
Checksum: 308
Coasting Arc #10 (Orbit 1353)
---------------------------------------
Vector Time (GMT): 2009/216/08:22:39
061
Vector Time (MET): N/A
Weight (LBS) : 672427
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4954543
51 A = 6727982
79 meter
Y = 2886338
85 meter E =
0003309
Z = -3515552
07 I = 51
93102
XDOT = -402
514360 Wp = 338
16331
YDOT = 6210
438744 meter/sec RA = 58
92222 deg
ZDOT = 4533
270637 TA = 340
23657
MA = 340
24939
Ha = 189
921 n
mi
Hp = 186
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16255064
02 X = 4938977
30
Y = 9469615
65 feet Y = 2941656
78 meter
Z = -11533963
48 Z = -3491520
92
XDOT = -1320
585169 XDOT = -493
951977
YDOT = 20375
455197 feet/sec YDOT = 6205
425876 meter/sec
ZDOT = 14872
935161 ZDOT = 4531
093799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12672183
86 X = 3862481
64
Y = -13981808
79 feet Y = -4261655
32 meter
Z = -11439310
28 Z = -3486701
77
XDOT = 18611
820328 XDOT = 5672
882836
YDOT = 4711
370970 feet/sec YDOT = 1436
025872 meter/sec
ZDOT = 14864
644362 ZDOT = 4530
743601
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 09216
35636468
00010596 00000-0 82463-4 0 9098
2 25544 51
6425 59
5385 0007230 298
8047 61
2396 15
73615189 13546
Satellite: ISS
Catalog Number: 25544
Epoch time: 09216
35636468 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node: 59
5385 deg
Eccentricity:
0007230
Arg of perigee: 298
8047 deg
Mean anomaly: 61
2396 deg
Mean motion: 15
73615189 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1354
Checksum: 334
Coasting Arc #11 (Orbit 1369)
---------------------------------------
Vector Time (GMT): 2009/217/08:22:39
061
Vector Time (MET): N/A
Weight (LBS) : 672427
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -235054
44 A = 6726674
51 meter
Y = -5488097
93 meter E =
0005830
Z = -3887165
88 I = 51
91056
XDOT = 5934
450344 Wp =
82362
YDOT = 2662
007205 meter/sec RA = 53
86084 deg
ZDOT = -4111
583722 TA = 226
39353
MA = 226
44192
Ha = 189
987 n
mi
Hp = 186
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -771175
97 X = -154785
39
Y = -18005570
65 feet Y = -5490277
32 meter
Z = -12753168
90 Z = -3888113
24
XDOT = 19469
981445 XDOT = 5924
215152
YDOT = 8733
619438 feet/sec YDOT = 2728
312823 meter/sec
ZDOT = -13489
447908 ZDOT = -4082
779437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17804059
71 X = -5426677
40
Y = -2776608
72 feet Y = -846310
34 meter
Z = -12757135
48 Z = -3888374
89
XDOT = 12125
078572 XDOT = 3695
723949
YDOT = -16206
988640 feet/sec YDOT = -4939
890137 meter/sec
ZDOT = -13376
026375 ZDOT = -4077
012839
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 09217
37244563
00010596 00000-0 82463-4 0 9104
2 25544 51
6427 54
3236 0007382 302
5596 57
4854 15
73626218 13705
Satellite: ISS
Catalog Number: 25544
Epoch time: 09217
37244563 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 54
3236 deg
Eccentricity:
0007382
Arg of perigee: 302
5596 deg
Mean anomaly: 57
4854 deg
Mean motion: 15
73626218 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1370
Checksum: 309
Coasting Arc #12 (Orbit 1385)
---------------------------------------
Vector Time (GMT): 2009/218/08:22:39
061
Vector Time (MET): N/A
Weight (LBS) : 672427
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5363186
94 A = 6727427
69 meter
Y = -1748875
73 meter E =
0008135
Z = 3665186
81 I = 51
89425
XDOT = -948
313644 Wp = 47
96114
YDOT = -6267
726879 meter/sec RA = 48
69478 deg
ZDOT = -4366
858971 TA = 88
21890
MA = 88
12573
Ha = 190
184 n
mi
Hp = 186
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17595757
69 X = -5361036
54
Y = -5737781
26 feet Y = -1808838
23 meter
Z = 12024891
12 Z = 3639138
13
XDOT = -3111
265235 XDOT = -856
943418
YDOT = -20563
408396 feet/sec YDOT = -6277
820329 meter/sec
ZDOT = -14326
965129 ZDOT = -4371
244236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8745178
86 X = -2665530
52
Y = 16386283
72 feet Y = 4994539
28 meter
Z = 11922347
99 Z = 3633931
67
XDOT = -19581
102046 XDOT = -5968
319904
YDOT = 14
217482 feet/sec YDOT = 4
333488 meter/sec
ZDOT = -14344
489761 ZDOT = -4372
200479
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 09218
38851662
00010596 00000-0 82463-4 0 9111
2 25544 51
6424 49
1082 0007363 307
4252 52
6241 15
73652949 13869
Satellite: ISS
Catalog Number: 25544
Epoch time: 09218
38851662 = yrday
fracday
Element set: 911
Inclination: 51
6424 deg
RA of node: 49
1082 deg
Eccentricity:
0007363
Arg of perigee: 307
4252 deg
Mean anomaly: 52
6241 deg
Mean motion: 15
73652949 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1386
Checksum: 310
Coasting Arc #13 (Orbit 1401)
---------------------------------------
Vector Time (GMT): 2009/219/08:22:39
061
Vector Time (MET): N/A
Weight (LBS) : 672427
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1411290
54 A = 6727081
16 meter
Y = 5403341
39 meter E =
0006943
Z = 3742307
14 I = 51
87275
XDOT = -6264
293272 Wp = 59
17995
YDOT = -1330
083780 meter/sec RA = 43
62986 deg
ZDOT = 4280
477311 TA = 345
86540
MA = 345
88482
Ha = 190
391 n
mi
Hp = 186
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4630218
30 X = 1332585
47
Y = 17727498
01 feet Y = 5418683
05 meter
Z = 12277910
58 Z = 3748972
11
XDOT = -20552
143281 XDOT = -6269
747848
YDOT = -4363
791929 feet/sec YDOT = -1400
165455 meter/sec
ZDOT = 14043
560731 ZDOT = 4250
032669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18225845
04 X = 5555237
57
Y = -1694510
68 feet Y = -516486
85 meter
Z = 12304365
14 Z = 3750370
49
XDOT = -7698
803257 XDOT = -2346
595233
YDOT = 18353
429495 feet/sec YDOT = 5594
125310 meter/sec
ZDOT = 13923
744588 ZDOT = 4243
957350
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 09219
40457698
00010596 00000-0 82463-4 0 9127
2 25544 51
6426 43
8921 0007439 311
6324 48
4201 15
73639993 14027
Satellite: ISS
Catalog Number: 25544
Epoch time: 09219
40457698 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 43
8921 deg
Eccentricity:
0007439
Arg of perigee: 311
6324 deg
Mean anomaly: 48
4201 deg
Mean motion: 15
73639993 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1402
Checksum: 314
Coasting Arc #14 (Orbit 1416)
---------------------------------------
Vector Time (GMT): 2009/220/08:22:39
061
Vector Time (MET): N/A
Weight (LBS) : 672427
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5516128
09 A = 6726904
56 meter
Y = 563586
77 meter E =
0003875
Z = -3805869
51 I = 51
84970
XDOT = 2282
520211 Wp = 6
57986
YDOT = 6032
011952 meter/sec RA = 38
46048 deg
ZDOT = 4205
654289 TA = 307
39729
MA = 307
43256
Ha = 190
605 n
mi
Hp = 186
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18097533
11 X = 5527903
92
Y = 1849037
96 feet Y = 625337
28 meter
Z = -12486448
53 Z = -3779043
98
XDOT = 7488
583368 XDOT = 2194
469603
YDOT = 19790
065460 feet/sec YDOT = 6057
044022 meter/sec
ZDOT = 13798
078376 ZDOT = 4216
528854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4397918
92 X = 1340485
69
Y = -17726323
61 feet Y = -5402983
44 meter
Z = -12380904
79 Z = -3773699
78
XDOT = 19345
934063 XDOT = 5896
640702
YDOT = -4857
870825 feet/sec YDOT = -1480
679028 meter/sec
ZDOT = 13841
118288 ZDOT = 4218
772854
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 09220
35712211
00010596 00000-0 82463-4 0 9139
2 25544 51
6424 39
0025 0007638 314
1851 45
8684 15
73675163 14172
Satellite: ISS
Catalog Number: 25544
Epoch time: 09220
35712211 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 39
0025 deg
Eccentricity:
0007638
Arg of perigee: 314
1851 deg
Mean anomaly: 45
8684 deg
Mean motion: 15
73675163 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1417
Checksum: 291
Coasting Arc #15 (Orbit 1432)
---------------------------------------
Vector Time (GMT): 2009/221/08:22:39
061
Vector Time (MET): N/A
Weight (LBS) : 672427
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2542318
48 A = 6727385
27 meter
Y = -5077931
28 meter E =
0006592
Z = -3613020
47 I = 51
82716
XDOT = 6299
293163 Wp = 1
98346
YDOT = -6
579719 meter/sec RA = 33
39310 deg
ZDOT = -4417
067227 TA = 221
08055
MA = 221
13021
Ha = 190
633 n
mi
Hp = 185
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8340939
90 X = -2467796
04
Y = -16659879
53 feet Y = -5105944
26 meter
Z = -11853741
70 Z = -3625189
94
XDOT = 20666
972321 XDOT = 6320
355617
YDOT = -21
587005 feet/sec YDOT = 63
980486 meter/sec
ZDOT = -14491
690377 ZDOT = -4386
414471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17558822
37 X = -5351929
06
Y = 6137445
76 feet Y = 1870693
47 meter
Z = -11901830
66 Z = -3627677
98
XDOT = 3004
475569 XDOT = 915
764153
YDOT = -19312
460738 feet/sec YDOT = -5886
438033 meter/sec
ZDOT = -14371
121182 ZDOT = -4380
317736
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 09221
37316089
00010596 00000-0 82463-4 0 9146
2 25544 51
6422 33
7872 0007691 317
4348 42
6218 15
73675857 14333
Satellite: ISS
Catalog Number: 25544
Epoch time: 09221
37316089 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 33
7872 deg
Eccentricity:
0007691
Arg of perigee: 317
4348 deg
Mean anomaly: 42
6218 deg
Mean motion: 15
73675857 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1433
Checksum: 319
Coasting Arc #16 (Orbit 1448)
---------------------------------------
Vector Time (GMT): 2009/222/08:22:39
061
Vector Time (MET): N/A
Weight (LBS) : 672427
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5444273
52 A = 6726345
27 meter
Y = 570113
18 meter E =
0010209
Z = 3909702
50 I = 51
79911
XDOT = -3507
599174 Wp = 37
77732
YDOT = -5514
384404 meter/sec RA = 28
22015 deg
ZDOT = -4066
756039 TA = 94
52606
MA = 94
40943
Ha = 190
790 n
mi
Hp = 185
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17861789
76 X = -5469236
48
Y = 1870450
07 feet Y = 509092
51 meter
Z = 12827107
95 Z = 3883193
79
XDOT = -11507
871305 XDOT = -3425
920272
YDOT = -18091
812350 feet/sec YDOT = -5553
151714 meter/sec
ZDOT = -13342
375456 ZDOT = -4083
597474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -62453
12 X = -19035
71
Y = 18033345
79 feet Y = 5496563
80 meter
Z = 12722867
38 Z = 3877929
98
XDOT = -17897
834707 XDOT = -5455
260019
YDOT = 9429
673545 feet/sec YDOT = 2874
164497 meter/sec
ZDOT = -13408
854974 ZDOT = -4087
018996
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 09222
38918749
00010596 00000-0 82463-4 0 9150
2 25544 51
6428 28
5714 0007850 322
2617 37
7994 15
73753564 14491
Satellite: ISS
Catalog Number: 25544
Epoch time: 09222
38918749 = yrday
fracday
Element set: 915
Inclination: 51
6428 deg
RA of node: 28
5714 deg
Eccentricity:
0007850
Arg of perigee: 322
2617 deg
Mean anomaly: 37
7994 deg
Mean motion: 15
73753564 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1449
Checksum: 341
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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