Date:
June 17th 2009
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) : 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
There are no maneuvers
Coasting Arc #1 (Orbit 568)
---------------------------------------
Vector Time (GMT): 2009/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4150385
13 A = 6721725
50 meter
Y = -1572017
23 meter E =
0021551
Z = -5066505
27 I = 51
38823
XDOT = 4310
246654 Wp = 92
80190
YDOT = -6150
172358 meter/sec RA = 315
00337 deg
ZDOT = -1629
622712 TA = 161
49102
MA = 161
41250
Ha = 193
686 n
mi
Hp = 180
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13616749
12 X = -4107885
88
Y = -5157536
85 feet Y = -1618191
03 meter
Z = -16622392
61 Z = -5086564
85
XDOT = 14141
229180 XDOT = 4386
615005
YDOT = -20177
730834 feet/sec YDOT = -6101
545467 meter/sec
ZDOT = -5346
531207 ZDOT = -1608
498725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6735968
49 X = -2053123
20
Y = 12807085
64 feet Y = 3903599
70 meter
Z = -16701055
80 Z = -5090481
81
XDOT = -17406
453655 XDOT = -5305
487074
YDOT = -15989
756513 feet/sec YDOT = -4873
677785 meter/sec
ZDOT = -5264
027602 ZDOT = -1604
475613
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 09166
51864541
00010596 00000-0 82463-4 0 9006
2 25544 51
6406 315
4687 0009075 116
5896 243
6198 15
73729774 5690
Satellite: ISS
Catalog Number: 25544
Epoch time: 09166
51864541 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 315
4687 deg
Eccentricity:
0009075
Arg of perigee: 116
5896 deg
Mean anomaly: 243
6198 deg
Mean motion: 15
73729774 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 569
Checksum: 346
Coasting Arc #2 (Orbit 584)
---------------------------------------
Vector Time (GMT): 2009/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3223680
65 A = 6732011
44 meter
Y = 5708979
51 meter E =
0022990
Z = 1478705
74 I = 51
40187
XDOT = -4939
030530 Wp = 119
19108
YDOT = -1277
918225 meter/sec RA = 309
82384 deg
ZDOT = -5777
333545 TA = 44
45835
MA = 44
27406
Ha = 193
599 n
mi
Hp = 181
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10576380
09 X = -3294463
17
Y = 18730247
74 feet Y = 5672534
48 meter
Z = 4851396
78 Z = 1462873
75
XDOT = -16204
168405 XDOT = -4896
308133
YDOT = -4192
645095 feet/sec YDOT = -1332
909781 meter/sec
ZDOT = -18954
506380 ZDOT = -5801
223891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17546450
00 X = 5348157
96
Y = 12465943
40 feet Y = 3799619
55 meter
Z = 4789613
15 Z = 1459874
09
XDOT = -4909
323955 XDOT = -1496
361941
YDOT = 14300
633254 feet/sec YDOT = 4358
833016 meter/sec
ZDOT = -19048
165897 ZDOT = -5805
880966
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 09167
53465257
00010596 00000-0 82463-4 0 9011
2 25544 51
6398 310
2518 0008948 120
8264 239
3780 15
73735141 5853
Satellite: ISS
Catalog Number: 25544
Epoch time: 09167
53465257 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 310
2518 deg
Eccentricity:
0008948
Arg of perigee: 120
8264 deg
Mean anomaly: 239
3780 deg
Mean motion: 15
73735141 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 585
Checksum: 324
Coasting Arc #3 (Orbit 600)
---------------------------------------
Vector Time (GMT): 2009/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4428560
04 A = 6721723
25 meter
Y = 639524
15 meter E =
0014171
Z = 5008109
85 I = 51
35078
XDOT = -3019
425698 Wp = 124
51875
YDOT = 6863
819798 meter/sec RA = 304
70034 deg
ZDOT = 1782
016064 TA = 308
19721
MA = 308
32475
Ha = 193
320 n
mi
Hp = 181
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14529396
44 X = 4396750
89
Y = 2098176
35 feet Y = 688868
40 meter
Z = 16430806
60 Z = 5029546
83
XDOT = -9906
252290 XDOT = -3104
610482
YDOT = 22519
093827 feet/sec YDOT = 6829
578292 meter/sec
ZDOT = 5846
509395 ZDOT = 1767
141516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3321107
11 X = 1012273
45
Y = -14202390
24 feet Y = -4328888
54 meter
Z = 16514825
75 Z = 5033718
89
XDOT = 20554
331314 XDOT = 6264
960185
YDOT = 11581
125417 feet/sec YDOT = 3529
927027 meter/sec
ZDOT = 5788
529445 ZDOT = 1764
343775
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 09168
55064427
00010596 00000-0 82463-4 0 9029
2 25544 51
6408 305
0363 0008826 124
6872 235
5124 15
73790491 6015
Satellite: ISS
Catalog Number: 25544
Epoch time: 09168
55064427 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 305
0363 deg
Eccentricity:
0008826
Arg of perigee: 124
6872 deg
Mean anomaly: 235
5124 deg
Mean motion: 15
73790491 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 601
Checksum: 304
Coasting Arc #4 (Orbit 615)
---------------------------------------
Vector Time (GMT): 2009/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2034459
22 A = 6731670
22 meter
Y = -6212395
36 meter E =
0011972
Z = -1614573
76 I = 51
36899
XDOT = 5138
275320 Wp = 85
15589
YDOT = 205
407883 meter/sec RA = 299
51700 deg
ZDOT = 5721
614833 TA = 256
96867
MA = 257
10235
Ha = 193
446 n
mi
Hp = 181
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6674734
96 X = 2111619
48
Y = -20381874
55 feet Y = -6189213
19 meter
Z = -5297158
02 Z = -1604503
73
XDOT = 16857
858660 XDOT = 5107
801596
YDOT = 673
910376 feet/sec YDOT = 262
695846 meter/sec
ZDOT = 18771
702208 ZDOT = 5746
502911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19878132
46 X = -6058854
77
Y = -8077520
71 feet Y = -2462028
31 meter
Z = -5257973
84 Z = -1602630
43
XDOT = 1223
982863 XDOT = 373
069977
YDOT = -15214
308586 feet/sec YDOT = -4637
321257 meter/sec
ZDOT = 18869
224783 ZDOT = 5751
339714
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 09169
50312479
00010596 00000-0 82463-4 0 9039
2 25544 51
6416 300
1469 0008890 127
4630 232
7343 15
73782172 6166
Satellite: ISS
Catalog Number: 25544
Epoch time: 09169
50312479 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 300
1469 deg
Eccentricity:
0008890
Arg of perigee: 127
4630 deg
Mean anomaly: 232
7343 deg
Mean motion: 15
73782172 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 616
Checksum: 305
Coasting Arc #5 (Orbit 631)
---------------------------------------
Vector Time (GMT): 2009/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4506775
79 A = 6721802
68 meter
Y = 253168
34 meter E =
0019622
Z = -4996766
65 I = 51
32260
XDOT = 1654
119626 Wp = 97
36296
YDOT = -7270
528809 meter/sec RA = 294
39267 deg
ZDOT = -1869
039579 TA = 154
53874
MA = 154
44195
Ha = 193
285 n
mi
Hp = 181
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14786009
80 X = -4484998
08
Y = 830604
78 feet Y = 202893
57 meter
Z = -16393591
36 Z = -5018607
93
XDOT = 5426
901661 XDOT = 1744
376554
YDOT = -23853
440973 feet/sec YDOT = -7251
526498 meter/sec
ZDOT = -6132
019615 ZDOT = -1860
785781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 81285
24 X = 24775
74
Y = 14713821
26 feet Y = 4484772
72 meter
Z = -16479159
09 Z = -5022847
69
XDOT = -22471
550966 XDOT = -6849
328734
YDOT = -6675
721645 feet/sec YDOT = -2034
759957 meter/sec
ZDOT = -6099
995790 ZDOT = -1859
278717
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 09170
51908870
00010596 00000-0 82463-4 0 9049
2 25544 51
6418 294
9313 0008755 131
2297 228
9622 15
73803568 6326
Satellite: ISS
Catalog Number: 25544
Epoch time: 09170
51908870 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 294
9313 deg
Eccentricity:
0008755
Arg of perigee: 131
2297 deg
Mean anomaly: 228
9622 deg
Mean motion: 15
73803568 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 632
Checksum: 325
Coasting Arc #6 (Orbit 647)
---------------------------------------
Vector Time (GMT): 2009/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -841666
42 A = 6731514
47 meter
Y = 6456260
48 meter E =
0022636
Z = 1661503
70 I = 51
34446
XDOT = -5117
510205 Wp = 123
22440
YDOT = 812
905625 meter/sec RA = 289
20540 deg
ZDOT = -5707
479689 TA = 38
31612
MA = 38
15551
Ha = 193
239 n
mi
Hp = 181
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2761372
76 X = -921870
24
Y = 21181956
96 feet Y = 6446399
70 meter
Z = 5451127
62 Z = 1657221
33
XDOT = -16789
731645 XDOT = -5098
493677
YDOT = 2667
013205 feet/sec YDOT = 755
786121 meter/sec
ZDOT = -18725
327065 ZDOT = -5732
294499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21075803
86 X = 6423905
02
Y = 3505793
39 feet Y = 1068565
82 meter
Z = 5434627
58 Z = 1656474
49
XDOT = 2358
212162 XDOT = 718
783067
YDOT = 15224
321803 feet/sec YDOT = 4640
373286 meter/sec
ZDOT = -18822
527077 ZDOT = -5737
106253
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 09171
53503866
00010596 00000-0 82463-4 0 9059
2 25544 51
6421 289
7151 0008820 135
0665 225
1214 15
73815994 6485
Satellite: ISS
Catalog Number: 25544
Epoch time: 09171
53503866 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 289
7151 deg
Eccentricity:
0008820
Arg of perigee: 135
0665 deg
Mean anomaly: 225
1214 deg
Mean motion: 15
73815994 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 648
Checksum: 314
Coasting Arc #7 (Orbit 663)
---------------------------------------
Vector Time (GMT): 2009/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4383582
47 A = 6721688
11 meter
Y = -1161549
52 meter E =
0014374
Z = 4955260
08 I = 51
30438
XDOT = -252
691848 Wp = 132
74604
YDOT = 7449
155067 meter/sec RA = 284
08051 deg
ZDOT = 1956
452663 TA = 298
19772
MA = 298
34281
Ha = 192
938 n
mi
Hp = 181
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14381832
25 X = 4372173
39
Y = -3810858
01 feet Y = -1112594
66 meter
Z = 16257414
95 Z = 4976527
70
XDOT = -829
041495 XDOT = -345
474940
YDOT = 24439
485129 feet/sec YDOT = 7445
810099 meter/sec
ZDOT = 6418
807951 ZDOT = 1955
001393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3573865
34 X = -1089314
16
Y = -14348241
92 feet Y = -4373344
14 meter
Z = 16340707
42 Z = 4980647
62
XDOT = 23375
650805 XDOT = 7124
898365
YDOT = 1530
788311 feet/sec YDOT = 466
584277 meter/sec
ZDOT = 6413
445117 ZDOT = 1954
818072
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 09172
55097213
00010596 00000-0 82463-4 0 9067
2 25544 51
6429 284
4994 0008663 138
7406 221
4413 15
73886293 6646
Satellite: ISS
Catalog Number: 25544
Epoch time: 09172
55097213 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 284
4994 deg
Eccentricity:
0008663
Arg of perigee: 138
7406 deg
Mean anomaly: 221
4413 deg
Mean motion: 15
73886293 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 664
Checksum: 333
Coasting Arc #8 (Orbit 678)
---------------------------------------
Vector Time (GMT): 2009/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -390378
19 A = 6731279
68 meter
Y = -6494484
47 meter E =
0010024
Z = -1736246
10 I = 51
33044
XDOT = 4875
189496 Wp = 93
52892
YDOT = -1801
683002 meter/sec RA = 278
89134 deg
ZDOT = 5670
690686 TA = 247
18789
MA = 247
29380
Ha = 193
008 n
mi
Hp = 181
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1280768
34 X = -309292
38
Y = -21307363
73 feet Y = -6498396
12 meter
Z = -5696345
48 Z = -1737947
14
XDOT = 15994
716195 XDOT = 4867
426706
YDOT = -5911
033472 feet/sec YDOT = -1747
210532 meter/sec
ZDOT = 18604
628235 ZDOT = 5694
355077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21306625
66 X = -6494259
50
Y = 1261963
61 feet Y = 384646
51 meter
Z = -5703299
00 Z = -1738365
53
XDOT = -5829
324740 XDOT = -1776
778181
YDOT = -14328
748632 feet/sec YDOT = -4367
402583 meter/sec
ZDOT = 18697
293769 ZDOT = 5698
935141
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 09173
50339949
00010596 00000-0 82463-4 0 9079
2 25544 51
6431 279
6101 0008510 141
1139 219
0637 15
73850278 6798
Satellite: ISS
Catalog Number: 25544
Epoch time: 09173
50339949 = yrday
fracday
Element set: 907
Inclination: 51
6431 deg
RA of node: 279
6101 deg
Eccentricity:
0008510
Arg of perigee: 141
1139 deg
Mean anomaly: 219
0637 deg
Mean motion: 15
73850278 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 679
Checksum: 317
Coasting Arc #9 (Orbit 694)
---------------------------------------
Vector Time (GMT): 2009/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4112162
99 A = 6721749
42 meter
Y = 1948541
15 meter E =
0017765
Z = -4961094
68 I = 51
29504
XDOT = -1105
540999 Wp = 102
06066
YDOT = -7347
227620 meter/sec RA = 273
76621 deg
ZDOT = -1979
000139 TA = 148
73458
MA = 148
62880
Ha = 192
851 n
mi
Hp = 181
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13491348
39 X = -4109546
37
Y = 6392851
53 feet Y = 1902572
30 meter
Z = -16276557
36 Z = -4981064
62
XDOT = -3627
103015 XDOT = -1013
687337
YDOT = -24105
077495 feet/sec YDOT = -7359
076392 meter/sec
ZDOT = -6492
782608 ZDOT = -1984
149389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6630958
03 X = 2021116
01
Y = 13280214
87 feet Y = 4047809
49 meter
Z = -16354743
66 Z = -4984925
87
XDOT = -23068
788391 XDOT = -7031
366701
YDOT = 3536
035633 feet/sec YDOT = 1077
783661 meter/sec
ZDOT = -6513
298792 ZDOT = -1985
253472
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 09174
51930703
00010596 00000-0 82463-4 0 9087
2 25544 51
6429 274
3945 0008514 145
7627 214
4087 15
73877209 6958
Satellite: ISS
Catalog Number: 25544
Epoch time: 09174
51930703 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 274
3945 deg
Eccentricity:
0008514
Arg of perigee: 145
7627 deg
Mean anomaly: 214
4087 deg
Mean motion: 15
73877209 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 695
Checksum: 335
Coasting Arc #10 (Orbit 710)
---------------------------------------
Vector Time (GMT): 2009/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1543901
58 A = 6731155
91 meter
Y = 6305367
09 meter E =
0021820
Z = 1732527
81 I = 51
32539
XDOT = -4480
402140 Wp = 127
56405
YDOT = 2667
144854 meter/sec RA = 268
57624 deg
ZDOT = -5678
602535 TA = 33
14950
MA = 33
01296
Ha = 192
792 n
mi
Hp = 181
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5065293
91 X = 1464862
96
Y = 20686899
90 feet Y = 6322189
61 meter
Z = 5684146
37 Z = 1739837
31
XDOT = -14699
482087 XDOT = -4482
308350
YDOT = 8750
475242 feet/sec YDOT = 2617
032891 meter/sec
ZDOT = -18630
585745 ZDOT = -5700
372133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20497809
87 X = 6247732
45
Y = -5754552
51 feet Y = -1753987
60 meter
Z = 5713095
99 Z = 1741351
66
XDOT = 8836
805818 XDOT = 2693
458413
YDOT = 12780
487154 feet/sec YDOT = 3895
492484 meter/sec
ZDOT = -18715
797797 ZDOT = -5704
575168
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 09175
53520129
00010596 00000-0 82463-4 0 9098
2 25544 51
6421 269
1791 0008597 148
5173 211
6506 15
73897647 7111
Satellite: ISS
Catalog Number: 25544
Epoch time: 09175
53520129 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 269
1791 deg
Eccentricity:
0008597
Arg of perigee: 148
5173 deg
Mean anomaly: 211
6506 deg
Mean motion: 15
73897647 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 711
Checksum: 329
Coasting Arc #11 (Orbit 726)
---------------------------------------
Vector Time (GMT): 2009/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3676453
53 A = 6721557
52 meter
Y = -2685307
20 meter E =
0013975
Z = 4940592
09 I = 51
29577
XDOT = 2424
346057 Wp = 140
75370
YDOT = 7032
896038 meter/sec RA = 263
45028 deg
ZDOT = 2004
702875 TA = 289
69397
MA = 289
84469
Ha = 192
517 n
mi
Hp = 181
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12061855
41 X = 3682207
71
Y = -8810062
98 feet Y = -2644163
64 meter
Z = 16209291
64 Z = 4958465
54
XDOT = 7953
891263 XDOT = 2335
784500
YDOT = 23073
805898 feet/sec YDOT = 7059
510966 meter/sec
ZDOT = 6577
109170 ZDOT = 2016
266300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9423082
72 X = -2872155
61
Y = -11490816
21 feet Y = -3502400
78 meter
Z = 16279230
81 Z = 4961909
55
XDOT = 21790
861977 XDOT = 6641
854731
YDOT = -8423
294144 feet/sec YDOT = -2567
420055 meter/sec
ZDOT = 6622
785515 ZDOT = 2018
625025
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 09176
55107923
00010596 00000-0 82463-4 0 9106
2 25544 51
6422 263
9626 0008427 152
6887 207
4721 15
73962577 7275
Satellite: ISS
Catalog Number: 25544
Epoch time: 09176
55107923 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 263
9626 deg
Eccentricity:
0008427
Arg of perigee: 152
6887 deg
Mean anomaly: 207
4721 deg
Mean motion: 15
73962577 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 727
Checksum: 331
Coasting Arc #12 (Orbit 741)
---------------------------------------
Vector Time (GMT): 2009/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2663308
14 A = 6731030
38 meter
Y = -5931926
21 meter E =
0008137
Z = -1750159
46 I = 51
33136
XDOT = 3918
381002 Wp = 100
92985
YDOT = -3424
459932 meter/sec RA = 258
25955 deg
ZDOT = 5664
722367 TA = 239
62623
MA = 239
70670
Ha = 192
507 n
mi
Hp = 182
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8737887
61 X = -2588276
55
Y = -19461700
17 feet Y = -5961289
10 meter
Z = -5741992
99 Z = -1762916
27
XDOT = 12855
580714 XDOT = 3928
864857
YDOT = -11235
104764 feet/sec YDOT = -3380
584526 meter/sec
ZDOT = 18585
047137 ZDOT = 5683
782561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18810555
70 X = -5733457
38
Y = 10034495
38 feet Y = 3058514
19 meter
Z = -5792308
15 Z = -1765495
53
XDOT = -11360
915582 XDOT = -3462
807069
YDOT = -10565
012110 feet/sec YDOT = -3220
215691 meter/sec
ZDOT = 18659
601103 ZDOT = 5687
446416
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 09177
50345493
00010596 00000-0 82463-4 0 9119
2 25544 51
6415 259
0728 0008175 155
6497 204
5054 15
73923521 7426
Satellite: ISS
Catalog Number: 25544
Epoch time: 09177
50345493 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 259
0728 deg
Eccentricity:
0008175
Arg of perigee: 155
6497 deg
Mean anomaly: 204
5054 deg
Mean motion: 15
73923521 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 742
Checksum: 315
Coasting Arc #13 (Orbit 757)
---------------------------------------
Vector Time (GMT): 2009/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3166452
89 A = 6721532
23 meter
Y = 3260198
83 meter E =
0016052
Z = -4964091
62 I = 51
30583
XDOT = -3616
860746 Wp = 106
10554
YDOT = -6495
401497 meter/sec RA = 253
13370 deg
ZDOT = -1968
463853 TA = 144
80385
MA = 144
69772
Ha = 192
357 n
mi
Hp = 182
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10388624
96 X = -3178559
24
Y = 10696190
39 feet Y = 3224722
65 meter
Z = -16286389
82 Z = -4979503
07
XDOT = -11866
341029 XDOT = -3534
396909
YDOT = -21310
372366 feet/sec YDOT = -6535
386015 meter/sec
ZDOT = -6458
214741 ZDOT = -1985
834919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11546919
28 X = 3519501
00
Y = 9329221
31 feet Y = 2843546
66 meter
Z = -16346644
79 Z = -4982457
33
XDOT = -19526
136348 XDOT = -5951
566359
YDOT = 12787
118205 feet/sec YDOT = 3897
513629 meter/sec
ZDOT = -6526
662531 ZDOT = -1989
326739
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 09178
51930875
00010596 00000-0 82463-4 0 9126
2 25544 51
6405 253
8560 0008250 159
7212 200
4280 15
73954884 7584
Satellite: ISS
Catalog Number: 25544
Epoch time: 09178
51930875 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 253
8560 deg
Eccentricity:
0008250
Arg of perigee: 159
7212 deg
Mean anomaly: 200
4280 deg
Mean motion: 15
73954884 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 758
Checksum: 320
Coasting Arc #14 (Orbit 773)
---------------------------------------
Vector Time (GMT): 2009/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3646894
97 A = 6730875
83 meter
Y = 5380777
66 meter E =
0020550
Z = 1699744
07 I = 51
34784
XDOT = -3280
152994 Wp = 132
19234
YDOT = 4031
403097 meter/sec RA = 247
94371 deg
ZDOT = -5694
004491 TA = 28
90605
MA = 28
79237
Ha = 192
160 n
mi
Hp = 182
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11964878
52 X = 3578198
16
Y = 17653470
02 feet Y = 5421175
06 meter
Z = 5576588
17 Z = 1717294
37
XDOT = -10761
656806 XDOT = -3297
328767
YDOT = 13226
388112 feet/sec YDOT = 3994
627164 meter/sec
ZDOT = -18681
117095 ZDOT = -5709
980609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16321053
07 X = 4974656
98
Y = -13698579
28 feet Y = -4175326
97 meter
Z = 5645689
47 Z = 1720806
15
XDOT = 13260
525164 XDOT = 4041
808070
YDOT = 8033
875073 feet/sec YDOT = 2448
725122 meter/sec
ZDOT = -18743
543691 ZDOT = -5713
032117
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 09179
53514916
00010596 00000-0 82463-4 0 9134
2 25544 51
6407 248
6393 0008117 162
1733 197
9716 15
74006695 7741
Satellite: ISS
Catalog Number: 25544
Epoch time: 09179
53514916 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 248
6393 deg
Eccentricity:
0008117
Arg of perigee: 162
1733 deg
Mean anomaly: 197
9716 deg
Mean motion: 15
74006695 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 774
Checksum: 335
Coasting Arc #15 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2009/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2542867
12 A = 6721292
52 meter
Y = -3746544
41 meter E =
0013024
Z = 4964724
53 I = 51
32804
XDOT = 4709
858186 Wp = 149
19526
YDOT = 5779
754376 meter/sec RA = 242
81846 deg
ZDOT = 1935
984384 TA = 281
95317
MA = 282
09915
Ha = 192
021 n
mi
Hp = 182
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8342739
90 X = 2560454
94
Y = -12291812
37 feet Y = -3718010
86 meter
Z = 16288466
30 Z = 4977120
01
XDOT = 15452
290635 XDOT = 4635
473299
YDOT = 18962
448739 feet/sec YDOT = 5832
006617 meter/sec
ZDOT = 6351
654804 ZDOT = 1958
684872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13197806
22 X = -4022691
34
Y = -6702890
71 feet Y = -2043041
09 meter
Z = 16336868
18 Z = 4979477
42
XDOT = 16472
935870 XDOT = 5020
950853
YDOT = -16630
359624 feet/sec YDOT = -5068
933613 meter/sec
ZDOT = 6440
979156 ZDOT = 1963
210447
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 09180
55097582
00010596 00000-0 82463-4 0 9144
2 25544 51
6407 243
4223 0008094 166
7610 193
3767 15
74030459 7903
Satellite: ISS
Catalog Number: 25544
Epoch time: 09180
55097582 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 243
4223 deg
Eccentricity:
0008094
Arg of perigee: 166
7610 deg
Mean anomaly: 193
3767 deg
Mean motion: 15
74030459 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 790
Checksum: 317
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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