Date:
January 7th 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
014/18:07:09
671 6
8 9
8 9
8
N/A 5
3 0
0 193
6
000/00:02:19
341 4
8 -0
1 192
9
Coasting Arc #1 (Orbit 2036)
---------------------------------------
Vector Time (GMT): 2009/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3780238
25 A = 6725736
74 meter
Y = 1742971
67 meter E =
0007039
Z = 5278836
74 I = 51
90428
XDOT = -3676
405083 Wp = 143
45136
YDOT = -6755
525633 meter/sec RA = 59
06444 deg
ZDOT = -407
428840 TA = 310
37219
MA = 310
43362
Ha = 194
826 n
mi
Hp = 185
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12402356
46 X = -3825091
20
Y = 5718411
01 feet Y = 1700447
62 meter
Z = 17319018
18 Z = 5260363
49
XDOT = -12061
696467 XDOT = -3598
611224
YDOT = -22163
798007 feet/sec YDOT = -6796
202321 meter/sec
ZDOT = -1336
708793 ZDOT = -425
100496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8658397
52 X = -2639079
56
Y = -10678575
95 feet Y = -3254829
95 meter
Z = 17247238
30 Z = 5256958
23
XDOT = 17674
467477 XDOT = 5387
177687
YDOT = -16573
546440 feet/sec YDOT = -5051
616955 meter/sec
ZDOT = -1405
908579 ZDOT = -428
520935
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 09005
54697578
00010596 00000-0 82463-4 0 9005
2 25544 51
6411 59
4499 0006743 165
7805 194
3548 15
72041805 20371
Satellite: ISS
Catalog Number: 25544
Epoch time: 09005
54697578 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 59
4499 deg
Eccentricity:
0006743
Arg of perigee: 165
7805 deg
Mean anomaly: 194
3548 deg
Mean motion: 15
72041805 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2037
Checksum: 326
Coasting Arc #2 (Orbit 2051)
---------------------------------------
Vector Time (GMT): 2009/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4140150
03 A = 6737818
46 meter
Y = 5306447
35 meter E =
0009657
Z = -288736
19 I = 51
92843
XDOT = -3588
406476 Wp = 76
68168
YDOT = 3119
488623 meter/sec RA = 53
96394 deg
ZDOT = 6047
410719 TA = 280
19737
MA = 280
30626
Ha = 194
662 n
mi
Hp = 185
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13583169
40 X = 4081907
39
Y = 17409604
17 feet Y = 5352419
29 meter
Z = -947297
21 Z = -268764
14
XDOT = -11772
987126 XDOT = -3652
399751
YDOT = 10234
542727 feet/sec YDOT = 3079
002508 meter/sec
ZDOT = 19840
586350 ZDOT = 6029
823077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13163285
06 X = -4012169
29
Y = 17733203
94 feet Y = 5405080
56 meter
Z = -869243
80 Z = -264945
51
XDOT = -11737
128828 XDOT = -3577
476867
YDOT = -7773
116898 feet/sec YDOT = -2369
246031 meter/sec
ZDOT = 19772
333134 ZDOT = 6026
607139
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 09006
50051127
00010596 00000-0 82463-4 0 9017
2 25544 51
6411 54
5672 0006516 167
4178 192
7148 15
72006144 20522
Satellite: ISS
Catalog Number: 25544
Epoch time: 09006
50051127 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 54
5672 deg
Eccentricity:
0006516
Arg of perigee: 167
4178 deg
Mean anomaly: 192
7148 deg
Mean motion: 15
72006144 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2052
Checksum: 279
Coasting Arc #3 (Orbit 2067)
---------------------------------------
Vector Time (GMT): 2009/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2338146
48 A = 6725991
25 meter
Y = -3554100
54 meter E =
0016074
Z = -5222149
11 I = 51
87161
XDOT = 5589
852268 Wp = 106
54740
YDOT = 5176
009699 meter/sec RA = 48
87243 deg
ZDOT = -1026
986047 TA = 153
71517
MA = 153
63352
Ha = 194
563 n
mi
Hp = 186
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7671084
26 X = 2403083
55
Y = -11660434
83 feet Y = -3527590
22 meter
Z = -17133035
13 Z = -5210633
13
XDOT = 18339
410327 XDOT = 5536
546747
YDOT = 16981
659116 feet/sec YDOT = 5238
220761 meter/sec
ZDOT = -3369
376794 ZDOT = -999
959246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13381844
60 X = 4078786
23
Y = 4154992
18 feet Y = 1266441
62 meter
Z = -17088430
07 Z = -5208553
48
XDOT = -10793
871547 XDOT = -3289
972047
YDOT = 21435
566884 feet/sec YDOT = 6533
560786 meter/sec
ZDOT = -3263
879832 ZDOT = -994
830573
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 09007
51760095
00010596 00000-0 82463-4 0 9021
2 25544 51
6420 49
3588 0006660 171
5255 188
6021 15
72049935 20688
Satellite: ISS
Catalog Number: 25544
Epoch time: 09007
51760095 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 49
3588 deg
Eccentricity:
0006660
Arg of perigee: 171
5255 deg
Mean anomaly: 188
6021 deg
Mean motion: 15
72049935 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2068
Checksum: 309
Coasting Arc #4 (Orbit 2083)
---------------------------------------
Vector Time (GMT): 2009/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5473118
95 A = 6736656
07 meter
Y = -3609494
84 meter E =
0018548
Z = 1500312
96 I = 51
88706
XDOT = 1569
723267 Wp = 135
17940
YDOT = -4808
517146 meter/sec RA = 43
74626 deg
ZDOT = -5811
766332 TA = 28
35014
MA = 28
24933
Ha = 194
410 n
mi
Hp = 186
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17956427
00 X = -5439638
44
Y = -11842174
66 feet Y = -3670511
47 meter
Z = 4922286
61 Z = 1473805
35
XDOT = 5150
010718 XDOT = 1651
608657
YDOT = -15775
974889 feet/sec YDOT = -4790
504800 meter/sec
ZDOT = -19067
474841 ZDOT = -5803
942520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5917649
76 X = 1803699
65
Y = -20704078
73 feet Y = -6310603
20 meter
Z = 4818902
56 Z = 1468801
50
XDOT = 15117
468661 XDOT = 4607
804448
YDOT = -133
766921 feet/sec YDOT = -40
772157 meter/sec
ZDOT = -19037
306139 ZDOT = -5802
570911
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 09008
53467539
00010596 00000-0 82463-4 0 9032
2 25544 51
6415 44
1507 0006550 174
1537 185
9703 15
72100997 20847
Satellite: ISS
Catalog Number: 25544
Epoch time: 09008
53467539 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 44
1507 deg
Eccentricity:
0006550
Arg of perigee: 174
1537 deg
Mean anomaly: 185
9703 deg
Mean motion: 15
72100997 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2084
Checksum: 309
Coasting Arc #5 (Orbit 2099)
---------------------------------------
Vector Time (GMT): 2009/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -305426
32 A = 6727324
48 meter
Y = 4644158
64 meter E =
0011831
Z = 4855866
04 I = 51
83308
XDOT = -6696
122498 Wp = 148
16408
YDOT = -2952
871306 meter/sec RA = 38
67324 deg
ZDOT = 2390
479518 TA = 278
50729
MA = 278
64135
Ha = 194
277 n
mi
Hp = 186
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1002054
87 X = -380924
05
Y = 15236740
94 feet Y = 4640320
21 meter
Z = 15931319
03 Z = 4854199
72
XDOT = -21968
905834 XDOT = -6674
217734
YDOT = -9687
897985 feet/sec YDOT = -3027
629164 meter/sec
ZDOT = 7842
780571 ZDOT = 2358
002772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14803350
68 X = -4512061
29
Y = 3771106
59 feet Y = 1149433
29 meter
Z = 15925102
14 Z = 4853971
13
XDOT = 2519
738550 XDOT = 768
016310
YDOT = -22866
688415 feet/sec YDOT = -6969
766629 meter/sec
ZDOT = 7716
194739 ZDOT = 2351
896156
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 09009
55173605
00010596 00000-0 82463-4 0 9044
2 25544 51
6408 38
9423 0006538 176
9908 183
1294 15
72111907 21002
Satellite: ISS
Catalog Number: 25544
Epoch time: 09009
55173605 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 38
9423 deg
Eccentricity:
0006538
Arg of perigee: 176
9908 deg
Mean anomaly: 183
1294 deg
Mean motion: 15
72111907 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2100
Checksum: 306
Coasting Arc #6 (Orbit 2114)
---------------------------------------
Vector Time (GMT): 2009/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6016704
60 A = 6734460
48 meter
Y = 1502578
44 meter E =
0005285
Z = -2634322
74 I = 51
83471
XDOT = 909
664467 Wp = 130
58980
YDOT = 5548
287042 meter/sec RA = 33
52510 deg
ZDOT = 5245
790396 TA = 199
59010
MA = 199
61042
Ha = 194
097 n
mi
Hp = 186
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19739844
49 X = 6012252
18
Y = 4929719
30 feet Y = 1569836
26 meter
Z = -8642791
16 Z = -2605104
68
XDOT = 2984
463476 XDOT = 822
072361
YDOT = 18203
041478 feet/sec YDOT = 5557
968817 meter/sec
ZDOT = 17210
598411 ZDOT = 5249
997627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1917711
64 X = 584518
51
Y = 20303708
24 feet Y = 6188570
27 meter
Z = -8528965
09 Z = -2599628
56
XDOT = -14733
278697 XDOT = -4490
703347
YDOT = 8623
366227 feet/sec YDOT = 2628
402026 meter/sec
ZDOT = 17227
296436 ZDOT = 5250
879954
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 09010
50521679
00010596 00000-0 82463-4 0 9050
2 25544 51
6419 34
0596 0006546 180
3274 179
7885 15
72168112 21159
Satellite: ISS
Catalog Number: 25544
Epoch time: 09010
50521679 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 34
0596 deg
Eccentricity:
0006546
Arg of perigee: 180
3274 deg
Mean anomaly: 179
7885 deg
Mean motion: 15
72168112 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2115
Checksum: 309
Coasting Arc #7 (Orbit 2130)
---------------------------------------
Vector Time (GMT): 2009/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1890376
19 A = 6729474
40 meter
Y = -4848693
54 meter E =
0008223
Z = -4270777
75 I = 51
79198
XDOT = 6796
811383 Wp = 113
95515
YDOT = 487
518319 meter/sec RA = 28
46203 deg
ZDOT = -3570
614565 TA = 119
88099
MA = 119
79926
Ha = 193
941 n
mi
Hp = 186
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6202021
64 X = -1815270
64
Y = -15907787
20 feet Y = -4869412
28 meter
Z = -14011738
01 Z = -4279779
23
XDOT = 22299
249945 XDOT = 6808
199703
YDOT = 1599
469551 feet/sec YDOT = 563
588379 meter/sec
ZDOT = -11714
614716 ZDOT = -3537
568714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12782617
62 X = 3896141
85
Y = -11275473
06 feet Y = -3436764
19 meter
Z = -14047062
40 Z = -4281544
62
XDOT = 5463
492759 XDOT = 1665
272593
YDOT = 20592
348820 feet/sec YDOT = 6276
547920 meter/sec
ZDOT = -11585
938135 ZDOT = -3531
393943
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 09011
52224865
00010596 00000-0 82463-4 0 9061
2 25544 51
6411 28
8504 0006430 185
0211 175
0888 15
72157029 21311
Satellite: ISS
Catalog Number: 25544
Epoch time: 09011
52224865 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 28
8504 deg
Eccentricity:
0006430
Arg of perigee: 185
0211 deg
Mean anomaly: 175
0888 deg
Mean motion: 15
72157029 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2131
Checksum: 282
Coasting Arc #8 (Orbit 2146)
---------------------------------------
Vector Time (GMT): 2009/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5657657
29 A = 6731833
64 meter
Y = 632199
41 meter E =
0012507
Z = 3578155
72 I = 51
77266
XDOT = -3408
981389 Wp = 116
12859
YDOT = -5284
560255 meter/sec RA = 23
29993 deg
ZDOT = -4449
923553 TA = 21
22975
MA = 21
17790
Ha = 193
847 n
mi
Hp = 186
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18561867
75 X = -5681687
73
Y = 2074145
04 feet Y = 568797
46 meter
Z = 11739356
05 Z = 3550613
25
XDOT = -11184
322142 XDOT = -3328
018859
YDOT = -17337
796111 feet/sec YDOT = -5322
228303 meter/sec
ZDOT = -14599
486723 ZDOT = -4466
287854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8715560
28 X = -2656502
77
Y = -16594855
36 feet Y = -5058111
91 meter
Z = 11632165
63 Z = 3545484
08
XDOT = 10895
484613 XDOT = 3320
943710
YDOT = -16015
856014 feet/sec YDOT = -4881
632913 meter/sec
ZDOT = -14663
505871 ZDOT = -4469
436589
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 09012
53926556
00010596 00000-0 82463-4 0 9070
2 25544 51
6402 23
6412 0006288 188
9483 171
1568 15
72202349 21471
Satellite: ISS
Catalog Number: 25544
Epoch time: 09012
53926556 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 23
6412 deg
Eccentricity:
0006288
Arg of perigee: 188
9483 deg
Mean anomaly: 171
1568 deg
Mean motion: 15
72202349 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2147
Checksum: 311
Coasting Arc #9 (Orbit 2162)
---------------------------------------
Vector Time (GMT): 2009/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3978854
00 A = 6732029
56 meter
Y = 4183173
85 meter E =
0012699
Z = 3459662
37 I = 51
74576
XDOT = -5918
106514 Wp = 120
58079
YDOT = 1838
842461 meter/sec RA = 18
23796 deg
ZDOT = 4564
137724 TA = 280
30756
MA = 280
45071
Ha = 193
584 n
mi
Hp = 186
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13053982
93 X = 3914975
36
Y = 13724323
65 feet Y = 4227310
28 meter
Z = 11350598
32 Z = 3478836
30
XDOT = -19416
359954 XDOT = -5960
400096
YDOT = 6032
947706 feet/sec YDOT = 1772
425950 meter/sec
ZDOT = 14974
205132 ZDOT = 4535
285704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7757316
57 X = -2364430
09
Y = 17230255
86 feet Y = 5251781
99 meter
Z = 11425494
95 Z = 3482490
86
XDOT = -11736
847915 XDOT = -3577
391245
YDOT = -15179
607687 feet/sec YDOT = -4626
744423 meter/sec
ZDOT = 14861
987457 ZDOT = 4529
933777
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 09013
55626847
00010596 00000-0 82463-4 0 9084
2 25544 51
6399 18
4323 0006325 193
3536 166
7459 15
72205919 21633
Satellite: ISS
Catalog Number: 25544
Epoch time: 09013
55626847 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 18
4323 deg
Eccentricity:
0006325
Arg of perigee: 193
3536 deg
Mean anomaly: 166
7459 deg
Mean motion: 15
72205919 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2163
Checksum: 327
Coasting Arc #10 (Orbit 2177)
---------------------------------------
Vector Time (GMT): 2009/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4519819
13 A = 6729243
45 meter
Y = -2469549
55 meter E =
0011073
Z = -4341639
37 I = 51
70790
XDOT = 5536
920297 Wp = 144
32173
YDOT = 4075
271544 meter/sec RA = 13
07232 deg
ZDOT = 3441
696681 TA = 160
47461
MA = 160
43217
Ha = 193
485 n
mi
Hp = 186
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14828802
93 X = 4568188
55
Y = -8102196
68 feet Y = -2418735
64 meter
Z = -14244223
66 Z = -4319565
21
XDOT = 18165
749007 XDOT = 5474
219655
YDOT = 13370
313465 feet/sec YDOT = 4136
837847 meter/sec
ZDOT = 11291
655778 ZDOT = 3468
442355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13344187
46 X = 4067308
34
Y = 10483716
53 feet Y = 3195436
80 meter
Z = -14158433
66 Z = -4315490
58
XDOT = -4346
050000 XDOT = -1324
676040
YDOT = 20942
086932 feet/sec YDOT = 6383
148097 meter/sec
ZDOT = 11396
025061 ZDOT = 3473
508439
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 09014
50969510
00010596 00000-0 82463-4 0 9098
2 25544 51
6401 13
5488 0006222 196
9691 163
1264 15
72198796 21787
Satellite: ISS
Catalog Number: 25544
Epoch time: 09014
50969510 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 13
5488 deg
Eccentricity:
0006222
Arg of perigee: 196
9691 deg
Mean anomaly: 163
1264 deg
Mean motion: 15
72198796 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2178
Checksum: 325
Coasting Arc #11 (Orbit 2181)
---------------------------------------
Vector Time (GMT): 2009/014/18:08:19
341
Vector Time (MET): N/A
Weight (LBS) : 639553
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5154193
65 A = 6736175
94 meter
Y = -2021418
96 meter E =
0003158
Z = -3837494
83 I = 51
70926
XDOT = 4799
309335 Wp = 219
14886
YDOT = 4347
402374 meter/sec RA = 11
76228 deg
ZDOT = 4151
753425 TA = 94
31490
MA = 94
27882
Ha = 193
591 n
mi
Hp = 192
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16910084
15 X = 5195055
88
Y = -6631951
98 feet Y = -1963553
13 meter
Z = -12590206
12 Z = -3812357
12
XDOT = 15745
765536 XDOT = 4730
171228
YDOT = 14263
131147 feet/sec YDOT = 4400
684270 meter/sec
ZDOT = 13621
238272 ZDOT = 4174
900251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12435955
77 X = 3790479
32
Y = -13331631
22 feet Y = -4063481
20 meter
Z = -12492463
19 Z = -3807702
78
XDOT = 19326
047025 XDOT = 5890
579133
YDOT = 5165
941388 feet/sec YDOT = 1574
578935 meter/sec
ZDOT = 13711
612829 ZDOT = 4179
299590
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 09014
76393920
00010596 00000-0 82463-4 0 9104
2 25544 51
6428 12
2470 0008092 263
8810 96
1430 15
70395973 21826
Satellite: ISS
Catalog Number: 25544
Epoch time: 09014
76393920 = yrday
fracday
Element set: 910
Inclination: 51
6428 deg
RA of node: 12
2470 deg
Eccentricity:
0008092
Arg of perigee: 263
8810 deg
Mean anomaly: 96
1430 deg
Mean motion: 15
70395973 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2182
Checksum: 300
Coasting Arc #12 (Orbit 2197)
---------------------------------------
Vector Time (GMT): 2009/015/18:08:19
341
Vector Time (MET): N/A
Weight (LBS) : 639553
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5504685
60 A = 6739234
76 meter
Y = -2792694
73 meter E =
0005092
Z = -2697059
60 I = 51
69130
XDOT = 4379
537220 Wp = 234
06958
YDOT = -3614
755932 meter/sec RA = 6
70705 deg
ZDOT = -5191
799936 TA = 336
61139
MA = 336
63454
Ha = 192
923 n
mi
Hp = 192
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18059992
14 X = -5459946
50
Y = -9162384
27 feet Y = -2854001
06 meter
Z = -8848620
74 Z = -2723692
36
XDOT = 14368
560432 XDOT = 4444
852929
YDOT = -11859
435473 feet/sec YDOT = -3565
416004 meter/sec
ZDOT = -17033
464357 ZDOT = -5170
365987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20205224
25 X = -6158552
35
Y = -113464
59 feet Y = -34584
01 meter
Z = -8952470
59 Z = -2728713
04
XDOT = 7603
524133 XDOT = 2317
554156
YDOT = -15614
343297 feet/sec YDOT = -4759
251837 meter/sec
ZDOT = -16950
239172 ZDOT = -5166
432900
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 09015
78210326
00010596 00000-0 82463-4 0 9116
2 25544 51
6434 7
0465 0008214 267
4945 92
5276 15
70393589 21980
Satellite: ISS
Catalog Number: 25544
Epoch time: 09015
78210326 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 7
0465 deg
Eccentricity:
0008214
Arg of perigee: 267
4945 deg
Mean anomaly: 92
5276 deg
Mean motion: 15
70393589 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2198
Checksum: 316
Coasting Arc #13 (Orbit 2213)
---------------------------------------
Vector Time (GMT): 2009/016/18:08:19
341
Vector Time (MET): N/A
Weight (LBS) : 639553
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2189632
56 A = 6731378
18 meter
Y = 3916718
03 meter E =
0004999
Z = 5021638
11 I = 51
63598
XDOT = -7272
475747 Wp = 314
45425
YDOT = -1673
827963 meter/sec RA = 1
56257 deg
ZDOT = -1863
256531 TA = 153
55446
MA = 153
52894
Ha = 192
906 n
mi
Hp = 192
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7183833
87 X = -2257661
11
Y = 12850124
76 feet Y = 3891851
70 meter
Z = 16475190
64 Z = 5010835
93
XDOT = -23859
828566 XDOT = -7244
166972
YDOT = -5491
561559 feet/sec YDOT = -1754
994644 meter/sec
ZDOT = -6113
046361 ZDOT = -1898
517085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -489170
47 X = -149099
16
Y = 14760420
53 feet Y = 4498976
18 meter
Z = 16433373
97 Z = 5008892
39
XDOT = -22577
757987 XDOT = -6881
700635
YDOT = 6219
008841 feet/sec YDOT = 1895
553895 meter/sec
ZDOT = -6250
412687 ZDOT = -1905
125787
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 09016
80025213
00010596 00000-0 82463-4 0 9120
2 25544 51
6433 1
8456 0008231 272
2756 87
7463 15
70471274 22145
Satellite: ISS
Catalog Number: 25544
Epoch time: 09016
80025213 = yrday
fracday
Element set: 912
Inclination: 51
6433 deg
RA of node: 1
8456 deg
Eccentricity:
0008231
Arg of perigee: 272
2756 deg
Mean anomaly: 87
7463 deg
Mean motion: 15
70471274 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2214
Checksum: 285
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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