Date:
August 11th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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 1450)
---------------------------------------
Vector Time (GMT): 2009/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1316147
76 A = 6721438
38 meter
Y = -3984886
51 meter E =
0011682
Z = -5259004
65 I = 51
77276
XDOT = 7008
874421 Wp = 53
77006
YDOT = 3114
388572 meter/sec RA = 27
49043 deg
ZDOT = -599
933317 TA = 210
49876
MA = 210
56675
Ha = 190
821 n
mi
Hp = 186
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4318070
09 X = 1386156
75
Y = -13073774
64 feet Y = -3969777
09 meter
Z = -17253952
25 Z = -5252440
83
XDOT = 22994
994821 XDOT = 6976
442227
YDOT = 10217
810277 feet/sec YDOT = 3192
584587 meter/sec
ZDOT = -1968
285161 ZDOT = -565
963191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11992259
20 X = -3655240
61
Y = 6829299
89 feet Y = 2081570
60 meter
Z = -17228307
04 Z = -5251187
99
XDOT = -9895
408878 XDOT = -3016
120626
YDOT = -22052
767143 feet/sec YDOT = -6721
683425 meter/sec
ZDOT = -1834
538970 ZDOT = -559
167478
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
51681966
00010596 00000-0 82463-4 0 9007
2 25544 51
6385 27
9292 0007843 316
8001 43
2545 15
73567394 14516
Satellite: ISS
Catalog Number: 25544
Epoch time: 09222
51681966 = yrday
fracday
Element set: 900
Inclination: 51
6385 deg
RA of node: 27
9292 deg
Eccentricity:
0007843
Arg of perigee: 316
8001 deg
Mean anomaly: 43
2545 deg
Mean motion: 15
73567394 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1451
Checksum: 313
Coasting Arc #2 (Orbit 1466)
---------------------------------------
Vector Time (GMT): 2009/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6371744
75 A = 6733135
73 meter
Y = -2073612
05 meter E =
0005551
Z = 642453
80 I = 51
78524
XDOT = 929
280194 Wp = 110
66922
YDOT = -4727
214823 meter/sec RA = 22
35623 deg
ZDOT = -6001
688253 TA = 62
35363
MA = 62
29730
Ha = 190
992 n
mi
Hp = 185
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20904674
37 X = -6351204
61
Y = -6803189
15 feet Y = -2144749
81 meter
Z = 2107788
05 Z = 611549
81
XDOT = 3048
819535 XDOT = 1011
226686
YDOT = -15509
234982 feet/sec YDOT = -4716
364776 meter/sec
ZDOT = -19690
578259 ZDOT = -5996
974857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11427507
09 X = 3483104
16
Y = 18793585
18 feet Y = 5728284
76 meter
Z = 1986152
36 Z = 605379
24
XDOT = -11138
373324 XDOT = -3394
976189
YDOT = 8866
324281 feet/sec YDOT = 2702
455641 meter/sec
ZDOT = -19672
240294 ZDOT = -5996
098842
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 09223
53293331
00010596 00000-0 82463-4 0 9016
2 25544 51
6383 22
7133 0008151 320
6668 39
3902 15
73605694 14672
Satellite: ISS
Catalog Number: 25544
Epoch time: 09223
53293331 = yrday
fracday
Element set: 901
Inclination: 51
6383 deg
RA of node: 22
7133 deg
Eccentricity:
0008151
Arg of perigee: 320
6668 deg
Mean anomaly: 39
3902 deg
Mean motion: 15
73605694 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1467
Checksum: 298
Coasting Arc #3 (Orbit 1482)
---------------------------------------
Vector Time (GMT): 2009/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -296791
37 A = 6721570
11 meter
Y = 4223066
07 meter E =
0005182
Z = 5221779
80 I = 51
71829
XDOT = -7480
975984 Wp = 339
54290
YDOT = -1600
052497 meter/sec RA = 17
24500 deg
ZDOT = 873
851861 TA = 102
17340
MA = 102
11535
Ha = 191
216 n
mi
Hp = 185
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -973724
95 X = -369358
81
Y = 13855203
65 feet Y = 4219341
26 meter
Z = 17131823
48 Z = 5220161
86
XDOT = -24543
884463 XDOT = -7466
772931
YDOT = -5249
516067 feet/sec YDOT = -1683
629777 meter/sec
ZDOT = 2866
968048 ZDOT = 837
543740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9675544
10 X = 2949105
84
Y = -9975502
26 feet Y = -3040533
09 meter
Z = 17125635
33 Z = 5219893
65
XDOT = 14817
562608 XDOT = 4516
393083
YDOT = 19020
365432 feet/sec YDOT = 5797
407384 meter/sec
ZDOT = 2724
102560 ZDOT = 830
306460
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 09224
54904269
00010596 00000-0 82463-4 0 9028
2 25544 51
6387 17
4979 0007968 324
9175 35
1462 15
73561725 14839
Satellite: ISS
Catalog Number: 25544
Epoch time: 09224
54904269 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 17
4979 deg
Eccentricity:
0007968
Arg of perigee: 324
9175 deg
Mean anomaly: 35
1462 deg
Mean motion: 15
73561725 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1483
Checksum: 337
Coasting Arc #4 (Orbit 1497)
---------------------------------------
Vector Time (GMT): 2009/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6627292
06 A = 6733026
79 meter
Y = 705345
28 meter E =
0014870
Z = -887196
90 I = 51
72956
XDOT = 276
306645 Wp = 8
51036
YDOT = 4871
026686 meter/sec RA = 12
10341 deg
ZDOT = 5963
648046 TA = 341
81377
MA = 341
86690
Ha = 191
298 n
mi
Hp = 185
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21743084
19 X = 6623222
05
Y = 2314124
93 feet Y = 779432
84 meter
Z = -2910750
99 Z = -855011
36
XDOT = 906
517864 XDOT = 192
847131
YDOT = 15981
058681 feet/sec YDOT = 4873
649537 meter/sec
ZDOT = 19565
774430 ZDOT = 5964
787886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15532425
67 X = -4734283
34
Y = -15413684
88 feet Y = -4698091
15 meter
Z = -2784138
46 Z = -848605
40
XDOT = 8251
909332 XDOT = 2515
181964
YDOT = -11833
678246 feet/sec YDOT = -3606
905129 meter/sec
ZDOT = 19570
454795 ZDOT = 5965
074621
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 09225
50163502
00010596 00000-0 82463-4 0 9033
2 25544 51
6401 12
6092 0007895 328
3045 31
7641 15
73591817 14984
Satellite: ISS
Catalog Number: 25544
Epoch time: 09225
50163502 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 12
6092 deg
Eccentricity:
0007895
Arg of perigee: 328
3045 deg
Mean anomaly: 31
7641 deg
Mean motion: 15
73591817 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1498
Checksum: 297
Coasting Arc #5 (Orbit 1513)
---------------------------------------
Vector Time (GMT): 2009/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -765033
40 A = 6721573
79 meter
Y = -4223569
13 meter E =
0014040
Z = -5183164
09 I = 51
66210
XDOT = 7606
810496 Wp = 48
69514
YDOT = 26
851315 meter/sec RA = 6
99402 deg
ZDOT = -1137
540240 TA = 210
39559
MA = 210
47707
Ha = 191
378 n
mi
Hp = 185
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2509952
09 X = -692569
04
Y = -13856854
08 feet Y = -4231718
62 meter
Z = -17005131
52 Z = -5186704
91
XDOT = 24956
727349 XDOT = 7611
470838
YDOT = 88
094867 feet/sec YDOT = 111
941276 meter/sec
ZDOT = -3732
087403 ZDOT = -1100
575101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6571698
89 X = -2003053
82
Y = 12435654
42 feet Y = 3790387
47 meter
Z = -17019225
47 Z = -5187459
92
XDOT = -18796
091857 XDOT = -5729
048798
YDOT = -14873
478187 feet/sec YDOT = -4533
436152 meter/sec
ZDOT = -3586
703074 ZDOT = -1093
227097
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 09226
51772629
00010596 00000-0 82463-4 0 9042
2 25544 51
6403 7
3953 0007961 332
7717 27
3027 15
73623638 15147
Satellite: ISS
Catalog Number: 25544
Epoch time: 09226
51772629 = yrday
fracday
Element set: 904
Inclination: 51
6403 deg
RA of node: 7
3953 deg
Eccentricity:
0007961
Arg of perigee: 332
7717 deg
Mean anomaly: 27
3027 deg
Mean motion: 15
73623638 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1514
Checksum: 309
Coasting Arc #6 (Orbit 1529)
---------------------------------------
Vector Time (GMT): 2009/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6610547
86 A = 6732767
04 meter
Y = 650363
03 meter E =
0008184
Z = 1090981
36 I = 51
66950
XDOT = -1445
067723 Wp = 91
75133
YDOT = -4718
069530 meter/sec RA = 1
84231 deg
ZDOT = -5905
732955 TA = 76
32509
MA = 76
23398
Ha = 191
532 n
mi
Hp = 184
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21688149
15 X = -6622628
78
Y = 2133736
98 feet Y = 576372
36 meter
Z = 3579335
18 Z = 1058838
22
XDOT = -4741
035838 XDOT = -1363
513249
YDOT = -15479
230743 feet/sec YDOT = -4733
772602 meter/sec
ZDOT = -19375
764289 ZDOT = -5912
555381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18673083
83 X = 5691555
95
Y = 11275346
59 feet Y = 3436725
64 meter
Z = 3452938
90 Z = 1052455
78
XDOT = -4728
245148 XDOT = -1441
169121
YDOT = 13811
626195 feet/sec YDOT = 4209
783664 meter/sec
ZDOT = -19402
782856 ZDOT = -5913
968215
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 09227
53380917
00010596 00000-0 82463-4 0 9051
2 25544 51
6399 2
1788 0008023 335
9482 24
1306 15
73622411 15305
Satellite: ISS
Catalog Number: 25544
Epoch time: 09227
53380917 = yrday
fracday
Element set: 905
Inclination: 51
6399 deg
RA of node: 2
1788 deg
Eccentricity:
0008023
Arg of perigee: 335
9482 deg
Mean anomaly: 24
1306 deg
Mean motion: 15
73622411 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1530
Checksum: 296
Coasting Arc #7 (Orbit 1545)
---------------------------------------
Vector Time (GMT): 2009/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1748437
19 A = 6721634
20 meter
Y = 3972784
15 meter E =
0005151
Z = 5130751
14 I = 51
60385
XDOT = -7427
891119 Wp = 6
63799
YDOT = 1509
562269 meter/sec RA = 356
73099 deg
ZDOT = 1367
272572 TA = 70
29838
MA = 70
24281
Ha = 191
601 n
mi
Hp = 184
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5736342
47 X = 1678958
91
Y = 13034068
75 feet Y = 3991947
26 meter
Z = 16833173
04 Z = 5139076
56
XDOT = -24369
721520 XDOT = -7450
861134
YDOT = 4952
632116 feet/sec YDOT = 1426
370675 meter/sec
ZDOT = 4485
802401 ZDOT = 1331
132628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3040192
85 X = 926650
78
Y = -13872311
38 feet Y = -4228280
51 meter
Z = 16866075
19 Z = 5140779
72
XDOT = 21680
214045 XDOT = 6608
129241
YDOT = 10012
987721 feet/sec YDOT = 3051
958657 meter/sec
ZDOT = 4343
714700 ZDOT = 1323
964241
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 09228
54988312
00010596 00000-0 82463-4 0 9067
2 25544 51
6411 356
9635 0008117 339
4770 20
6066 15
73661234 15461
Satellite: ISS
Catalog Number: 25544
Epoch time: 09228
54988312 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 356
9635 deg
Eccentricity:
0008117
Arg of perigee: 339
4770 deg
Mean anomaly: 20
6066 deg
Mean motion: 15
73661234 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1546
Checksum: 318
Coasting Arc #8 (Orbit 1560)
---------------------------------------
Vector Time (GMT): 2009/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6293905
23 A = 6732519
96 meter
Y = -1974049
54 meter E =
0015410
Z = -1300502
93 I = 51
61107
XDOT = 2555
657363 Wp = 11
81606
YDOT = 4309
669974 meter/sec RA = 351
57289 deg
ZDOT = 5853
611409 TA = 333
89647
MA = 333
97408
Ha = 191
882 n
mi
Hp = 184
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20649295
37 X = 6321829
12
Y = -6476540
48 feet Y = -1903511
16 meter
Z = -4266741
90 Z = -1269859
99
XDOT = 8384
702634 XDOT = 2478
840651
YDOT = 14139
337185 feet/sec YDOT = 4337
818862 meter/sec
ZDOT = 19204
761840 ZDOT = 5865
840342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20676258
45 X = -6302123
58
Y = -6468746
25 feet Y = -1971673
86 meter
Z = -4146290
00 Z = -1263789
19
XDOT = 795
536752 XDOT = 242
479602
YDOT = -14825
104618 feet/sec YDOT = -4518
691888 meter/sec
ZDOT = 19253
035082 ZDOT = 5868
325093
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 09229
50244648
00010596 00000-0 82463-4 0 9072
2 25544 51
6418 352
0748 0008173 344
0849 16
0056 15
73635381 15610
Satellite: ISS
Catalog Number: 25544
Epoch time: 09229
50244648 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 352
0748 deg
Eccentricity:
0008173
Arg of perigee: 344
0849 deg
Mean anomaly: 16
0056 deg
Mean motion: 15
73635381 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1561
Checksum: 312
Coasting Arc #9 (Orbit 1576)
---------------------------------------
Vector Time (GMT): 2009/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2671784
95 A = 6721879
10 meter
Y = -3509857
80 meter E =
0015967
Z = -5084654
46 I = 51
54650
XDOT = 6918
120930 Wp = 46
82886
YDOT = -2959
931282 meter/sec RA = 346
46170 deg
ZDOT = -1584
394378 TA = 207
87397
MA = 207
95960
Ha = 191
920 n
mi
Hp = 184
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8765698
65 X = -2607638
74
Y = -11515281
51 feet Y = -3539376
34 meter
Z = -16681937
21 Z = -5097478
10
XDOT = 22697
247145 XDOT = 6958
401758
YDOT = -9711
060635 feet/sec YDOT = -2882
343486 meter/sec
ZDOT = -5198
144285 ZDOT = -1550
689180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 801838
73 X = 244400
45
Y = 14391175
66 feet Y = 4386430
34 meter
Z = -16732523
06 Z = -5100073
03
XDOT = -23240
208986 XDOT = -7083
615699
YDOT = -4623
897973 feet/sec YDOT = -1409
364102 meter/sec
ZDOT = -5065
686281 ZDOT = -1544
021178
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 09230
51850500
00010596 00000-0 82463-4 0 9086
2 25544 51
6421 346
8602 0008227 347
5492 12
5467 15
73655785 15770
Satellite: ISS
Catalog Number: 25544
Epoch time: 09230
51850500 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 346
8602 deg
Eccentricity:
0008227
Arg of perigee: 347
5492 deg
Mean anomaly: 12
5467 deg
Mean motion: 15
73655785 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1577
Checksum: 316
Coasting Arc #10 (Orbit 1592)
---------------------------------------
Vector Time (GMT): 2009/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5754254
86 A = 6732249
27 meter
Y = 3172221
28 meter E =
0011152
Z = 1460309
17 I = 51
55283
XDOT = -3501
071742 Wp = 83
10103
YDOT = -3667
564564 meter/sec RA = 341
29569 deg
ZDOT = -5789
674900 TA = 80
81697
MA = 80
69084
Ha = 192
059 n
mi
Hp = 184
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18878788
91 X = -5796393
27
Y = 10407550
13 feet Y = 3107638
19 meter
Z = 4791040
58 Z = 1432253
35
XDOT = -11486
455848 XDOT = -3431
675645
YDOT = -12032
692138 feet/sec YDOT = -3706
327470 meter/sec
ZDOT = -18994
996390 ZDOT = -5806
514236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21530068
87 X = 6562364
99
Y = 1491954
60 feet Y = 454747
76 meter
Z = 4680816
85 Z = 1426712
98
XDOT = 3153
498283 XDOT = 961
186277
YDOT = 14706
594021 feet/sec YDOT = 4482
569858 meter/sec
ZDOT = -19061
390018 ZDOT = -5809
911677
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 09231
53455562
00010596 00000-0 82463-4 0 9099
2 25544 51
6423 341
6449 0008170 351
8712 8
2318 15
73663234 15937
Satellite: ISS
Catalog Number: 25544
Epoch time: 09231
53455562 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 341
6449 deg
Eccentricity:
0008170
Arg of perigee: 351
8712 deg
Mean anomaly: 8
2318 deg
Mean motion: 15
73663234 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1593
Checksum: 306
Coasting Arc #11 (Orbit 1608)
---------------------------------------
Vector Time (GMT): 2009/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3418405
83 A = 6721885
25 meter
Y = 2862377
56 meter E =
0006345
Z = 5025955
19 I = 51
49148
XDOT = -6168
059956 Wp = 34
33135
YDOT = 4263
263225 meter/sec RA = 336
18244 deg
ZDOT = 1771
274533 TA = 38
60563
MA = 38
56028
Ha = 192
042 n
mi
Hp = 183
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11215242
22 X = 3361729
49
Y = 9391002
49 feet Y = 2900287
34 meter
Z = 16489354
30 Z = 5042423
77
XDOT = -20236
417179 XDOT = -6223
878429
YDOT = 13987
084070 feet/sec YDOT = 4193
976276 meter/sec
ZDOT = 5811
268152 ZDOT = 1741
175094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4498646
73 X = -1371187
52
Y = -13841607
42 feet Y = -4218921
94 meter
Z = 16554258
44 Z = 5045737
97
XDOT = 23588
759249 XDOT = 7189
853819
YDOT = -873
712474 feet/sec YDOT = -266
307562 meter/sec
ZDOT = 5693
060207 ZDOT = 1735
244751
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 09232
55059611
00010596 00000-0 82463-4 0 9109
2 25544 51
6430 336
4297 0008287 355
5276 4
5812 15
73718025 16098
Satellite: ISS
Catalog Number: 25544
Epoch time: 09232
55059611 = yrday
fracday
Element set: 910
Inclination: 51
6430 deg
RA of node: 336
4297 deg
Eccentricity:
0008287
Arg of perigee: 355
5276 deg
Mean anomaly: 4
5812 deg
Mean motion: 15
73718025 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1609
Checksum: 307
Coasting Arc #12 (Orbit 1623)
---------------------------------------
Vector Time (GMT): 2009/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4958939
30 A = 6732005
99 meter
Y = -4235271
92 meter E =
0015641
Z = -1635799
44 I = 51
49810
XDOT = 4299
423407 Wp = 17
36119
YDOT = 2831
087559 meter/sec RA = 331
01032 deg
ZDOT = 5732
435881 TA = 324
52594
MA = 324
62986
Ha = 192
423 n
mi
Hp = 183
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16269485
88 X = 5013876
57
Y = -13895249
07 feet Y = -4179511
02 meter
Z = -5366796
05 Z = -1611575
72
XDOT = 14105
719839 XDOT = 4239
599460
YDOT = 9288
345010 feet/sec YDOT = 2878
831922 meter/sec
ZDOT = 18807
204333 ZDOT = 5753
176749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21118012
83 X = -6436770
31
Y = 3579839
81 feet Y = 1091135
17 meter
Z = -5271707
36 Z = -1606816
40
XDOT = -6998
139065 XDOT = -2133
032787
YDOT = -13608
279123 feet/sec YDOT = -4147
803477 meter/sec
ZDOT = 18888
912403 ZDOT = 5757
340500
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 09233
50312898
00010596 00000-0 82463-4 0 9115
2 25544 51
6430 331
5414 0008542 359
3427
7723 15
73664775 16247
Satellite: ISS
Catalog Number: 25544
Epoch time: 09233
50312898 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 331
5414 deg
Eccentricity:
0008542
Arg of perigee: 359
3427 deg
Mean anomaly:
7723 deg
Mean motion: 15
73664775 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1624
Checksum: 302
Coasting Arc #13 (Orbit 1639)
---------------------------------------
Vector Time (GMT): 2009/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4031280
59 A = 6722199
53 meter
Y = -2066000
17 meter E =
0017550
Z = -4981407
73 I = 51
43944
XDOT = 5156
414705 Wp = 48
07797
YDOT = -5361
376014 meter/sec RA = 325
89663 deg
ZDOT = -1942
171568 TA = 203
03394
MA = 203
11272
Ha = 192
397 n
mi
Hp = 183
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13225986
18 X = -3983680
07
Y = -6778215
79 feet Y = -2110814
36 meter
Z = -16343201
22 Z = -5000875
80
XDOT = 16917
371079 XDOT = 5225
417921
YDOT = -17589
816318 feet/sec YDOT = -5303
328212 meter/sec
ZDOT = -6371
953962 ZDOT = -1916
954146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8017020
71 X = 2443587
91
Y = 12413158
23 feet Y = 3783530
63 meter
Z = -16419866
85 Z = -5004775
42
XDOT = -22553
495784 XDOT = -6874
305515
YDOT = 6237
456210 feet/sec YDOT = 1901
176653 meter/sec
ZDOT = -6273
016294 ZDOT = -1912
015366
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 09234
51915481
00010596 00000-0 82463-4 0 9125
2 25544 51
6426 326
3266 0008411 2
8662 357
2548 15
73692081 16409
Satellite: ISS
Catalog Number: 25544
Epoch time: 09234
51915481 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 326
3266 deg
Eccentricity:
0008411
Arg of perigee: 2
8662 deg
Mean anomaly: 357
2548 deg
Mean motion: 15
73692081 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1640
Checksum: 304
Coasting Arc #14 (Orbit 1655)
---------------------------------------
Vector Time (GMT): 2009/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4027359
89 A = 6731687
42 meter
Y = 5099210
02 meter E =
0014133
Z = 1753015
07 I = 51
44673
XDOT = -4854
447945 Wp = 79
89430
YDOT = -1869
747415 meter/sec RA = 320
71764 deg
ZDOT = -5672
600487 TA = 80
65030
MA = 80
49053
Ha = 192
554 n
mi
Hp = 183
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13213122
99 X = -4092596
60
Y = 16729691
68 feet Y = 5053809
02 meter
Z = 5751361
77 Z = 1733291
62
XDOT = -15926
666485 XDOT = -4805
622978
YDOT = -6134
341912 feet/sec YDOT = -1923
759897 meter/sec
ZDOT = -18610
893987 ZDOT = -5696
064622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19675283
01 X = 5997026
26
Y = -8260510
32 feet Y = -2517803
55 meter
Z = 5674026
15 Z = 1729443
17
XDOT = 10291
484480 XDOT = 3136
844469
YDOT = 11571
644179 feet/sec YDOT = 3527
037146 meter/sec
ZDOT = -18703
264777 ZDOT = -5700
755104
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 09235
53517270
00010596 00000-0 82463-4 0 9133
2 25544 51
6418 321
1115 0008497 7
9672 352
1625 15
73715421 16568
Satellite: ISS
Catalog Number: 25544
Epoch time: 09235
53517270 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 321
1115 deg
Eccentricity:
0008497
Arg of perigee: 7
9672 deg
Mean anomaly: 352
1625 deg
Mean motion: 15
73715421 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1656
Checksum: 301
Coasting Arc #15 (Orbit 1671)
---------------------------------------
Vector Time (GMT): 2009/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4414351
27 A = 6722188
03 meter
Y = 1179371
18 meter E =
0008320
Z = 4923263
71 I = 51
39320
XDOT = -3996
933386 Wp = 52
68559
YDOT = 6248
973479 meter/sec RA = 315
60103 deg
ZDOT = 2089
388452 TA = 17
02778
MA = 16
99988
Ha = 192
454 n
mi
Hp = 182
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14482779
76 X = 4376918
96
Y = 3869328
01 feet Y = 1228525
85 meter
Z = 16152439
98 Z = 4944617
65
XDOT = -13113
298509 XDOT = -4076
663276
YDOT = 20501
881492 feet/sec YDOT = 6203
831670 meter/sec
ZDOT = 6854
948989 ZDOT = 2069
777591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10910978
74 X = -3325666
32
Y = -10146490
55 feet Y = -3092650
32 meter
Z = 16236477
41 Z = 4948878
31
XDOT = 20471
090563 XDOT = 6239
588404
YDOT = -11180
476726 feet/sec YDOT = -3407
809306 meter/sec
ZDOT = 6778
112762 ZDOT = 2065
968770
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 09236
55118030
00010596 00000-0 82463-4 0 9148
2 25544 51
6420 315
8954 0008536 10
9601 349
1746 15
73757324 16728
Satellite: ISS
Catalog Number: 25544
Epoch time: 09236
55118030 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 315
8954 deg
Eccentricity:
0008536
Arg of perigee: 10
9601 deg
Mean anomaly: 349
1746 deg
Mean motion: 15
73757324 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1672
Checksum: 306
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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