Date:
June 12th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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 489)
---------------------------------------
Vector Time (GMT): 2009/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5978327
07 A = 6732982
19 meter
Y = -2928241
46 meter E =
0016277
Z = -992449
61 I = 51
54772
XDOT = 2910
496425 Wp = 66
27452
YDOT = 3963
147720 meter/sec RA = 340
70284 deg
ZDOT = 5921
733089 TA = 282
87246
MA = 283
05424
Ha = 193
981 n
mi
Hp = 181
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19613933
97 X = 6015447
97
Y = -9607091
41 feet Y = -2861180
58 meter
Z = -3256068
26 Z = -963317
33
XDOT = 9548
872785 XDOT = 2837
196875
YDOT = 13002
453151 feet/sec YDOT = 3995
283631 meter/sec
ZDOT = 19428
258165 ZDOT = 5935
694961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5393451
56 X = -1643924
03
Y = -21181191
29 feet Y = -6456027
11 meter
Z = -3142038
74 Z = -957693
41
XDOT = 13111
798474 XDOT = 3996
476175
YDOT = -6187
093677 feet/sec YDOT = -1885
826153 meter/sec
ZDOT = 19483
112832 ZDOT = 5938
452791
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 09161
50184860
00010596 00000-0 82463-4 0 9009
2 25544 51
6384 341
2153 0008852 98
7985 261
4181 15
73574283 4908
Satellite: ISS
Catalog Number: 25544
Epoch time: 09161
50184860 = yrday
fracday
Element set: 900
Inclination: 51
6384 deg
RA of node: 341
2153 deg
Eccentricity:
0008852
Arg of perigee: 98
7985 deg
Mean anomaly: 261
4181 deg
Mean motion: 15
73574283 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 490
Checksum: 317
Coasting Arc #2 (Orbit 505)
---------------------------------------
Vector Time (GMT): 2009/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2956886
17 A = 6721703
75 meter
Y = -3166900
10 meter E =
0022893
Z = -5158725
57 I = 51
48259
XDOT = 6439
494852 Wp = 88
70247
YDOT = -4004
690935 meter/sec RA = 335
58141 deg
ZDOT = -1236
767336 TA = 169
44939
MA = 169
40127
Ha = 193
940 n
mi
Hp = 181
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9701070
12 X = -2896193
55
Y = -10390092
18 feet Y = -3199625
47 meter
Z = -16924952
65 Z = -5172943
20
XDOT = 21126
951615 XDOT = 6489
805353
YDOT = -13138
749788 feet/sec YDOT = -3932
399226 meter/sec
ZDOT = -4057
635618 ZDOT = -1205
362890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12006138
90 X = -3659471
14
Y = 7484947
83 feet Y = 2281412
10 meter
Z = -16980782
78 Z = -5175742
59
XDOT = -8395
800954 XDOT = -2559
040131
YDOT = -22362
497485 feet/sec YDOT = -6816
089234 meter/sec
ZDOT = -3934
744862 ZDOT = -1199
310234
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 09162
51794647
00010596 00000-0 82463-4 0 9012
2 25544 51
6386 336
0002 0008986 102
4239 257
7930 15
73607218 5061
Satellite: ISS
Catalog Number: 25544
Epoch time: 09162
51794647 = yrday
fracday
Element set: 901
Inclination: 51
6386 deg
RA of node: 336
0002 deg
Eccentricity:
0008986
Arg of perigee: 102
4239 deg
Mean anomaly: 257
7930 deg
Mean motion: 15
73607218 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 506
Checksum: 313
Coasting Arc #3 (Orbit 521)
---------------------------------------
Vector Time (GMT): 2009/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5240568
55 A = 6732571
43 meter
Y = 4045837
51 meter E =
0022295
Z = 1170276
10 I = 51
49302
XDOT = -3810
047681 Wp = 115
50413
YDOT = -3213
104092 meter/sec RA = 330
41585 deg
ZDOT = -5876
114667 TA = 51
64364
MA = 51
44350
Ha = 193
736 n
mi
Hp = 181
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17193466
36 X = -5291105
26
Y = 13273745
11 feet Y = 3986951
66 meter
Z = 3839488
53 Z = 1144695
42
XDOT = -12500
156433 XDOT = -3745
290069
YDOT = -10541
680092 feet/sec YDOT = -3255
347261 meter/sec
ZDOT = -19278
591426 ZDOT = -5894
467009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10143945
75 X = 3091874
66
Y = 19226709
76 feet Y = 5860301
14 meter
Z = 3739420
16 Z = 1139775
27
XDOT = -11097
928005 XDOT = -3382
648456
YDOT = 9669
383019 feet/sec YDOT = 2947
227944 meter/sec
ZDOT = -19350
627685 ZDOT = -5898
071318
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 09163
53402461
00010596 00000-0 82463-4 0 9026
2 25544 51
6385 330
7841 0008693 105
2496 254
9629 15
73665148 5221
Satellite: ISS
Catalog Number: 25544
Epoch time: 09163
53402461 = yrday
fracday
Element set: 902
Inclination: 51
6385 deg
RA of node: 330
7841 deg
Eccentricity:
0008693
Arg of perigee: 105
2496 deg
Mean anomaly: 254
9629 deg
Mean motion: 15
73665148 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 522
Checksum: 317
Coasting Arc #4 (Orbit 537)
---------------------------------------
Vector Time (GMT): 2009/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3662571
38 A = 6721797
51 meter
Y = 2400727
24 meter E =
0013307
Z = 5090260
20 I = 51
43131
XDOT = -5477
784790 Wp = 114
50450
YDOT = 5220
512934 meter/sec RA = 325
29376 deg
ZDOT = 1470
798885 TA = 321
32329
MA = 321
41851
Ha = 193
707 n
mi
Hp = 181
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12016310
29 X = 3610726
36
Y = 7876401
71 feet Y = 2441393
65 meter
Z = 16700328
73 Z = 5107927
31
XDOT = -17971
734874 XDOT = -5542
899176
YDOT = 17127
667105 feet/sec YDOT = 5158
892862 meter/sec
ZDOT = 4825
455661 ZDOT = 1444
030477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9613350
03 X = 2930149
09
Y = -10568477
79 feet Y = -3221272
03 meter
Z = 16769650
42 Z = 5111389
45
XDOT = 13390
373370 XDOT = 4081
385803
YDOT = 19714
771892 feet/sec YDOT = 6009
062473 meter/sec
ZDOT = 4720
785475 ZDOT = 1438
895413
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 09164
55008880
00010596 00000-0 82463-4 0 9037
2 25544 51
6384 325
5687 0008861 109
5506 250
6615 15
73641914 5386
Satellite: ISS
Catalog Number: 25544
Epoch time: 09164
55008880 = yrday
fracday
Element set: 903
Inclination: 51
6384 deg
RA of node: 325
5687 deg
Eccentricity:
0008861
Arg of perigee: 109
5506 deg
Mean anomaly: 250
6615 deg
Mean motion: 15
73641914 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 538
Checksum: 323
Coasting Arc #5 (Orbit 552)
---------------------------------------
Vector Time (GMT): 2009/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4280405
80 A = 6732268
16 meter
Y = -5009778
91 meter E =
0013941
Z = -1380236
35 I = 51
44429
XDOT = 4508
564578 Wp = 75
50520
YDOT = 2266
186033 meter/sec RA = 320
12133 deg
ZDOT = 5808
866464 TA = 269
29614
MA = 269
45588
Ha = 193
758 n
mi
Hp = 181
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14043326
10 X = 4342812
79
Y = -16436282
51 feet Y = -4961563
80 meter
Z = -4528334
48 Z = -1359291
21
XDOT = 14791
878538 XDOT = 4454
670230
YDOT = 7434
993545 feet/sec YDOT = 2316
301354 meter/sec
ZDOT = 19057
960841 ZDOT = 5830
638427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14361734
73 X = -4377456
75
Y = -16181520
77 feet Y = -4932127
53 meter
Z = -4446477
83 Z = -1355286
44
XDOT = 8189
966305 XDOT = 2496
301730
YDOT = -12481
234648 feet/sec YDOT = -3804
280321 meter/sec
ZDOT = 19143
362195 ZDOT = 5834
896797
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 09165
50263035
00010596 00000-0 82463-4 0 9049
2 25544 51
6396 320
6794 0008939 113
6431 246
5671 15
73683963 5536
Satellite: ISS
Catalog Number: 25544
Epoch time: 09165
50263035 = yrday
fracday
Element set: 904
Inclination: 51
6396 deg
RA of node: 320
6794 deg
Eccentricity:
0008939
Arg of perigee: 113
6431 deg
Mean anomaly: 246
5671 deg
Mean motion: 15
73683963 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 553
Checksum: 325
Coasting Arc #6 (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 = -4155203
50 A = 6721749
83 meter
Y = -1565034
62 meter E =
0021383
Z = -5064613
45 I = 51
38750
XDOT = 4303
988853 Wp = 92
67171
YDOT = -6152
778400 meter/sec RA = 314
99946 deg
ZDOT = -1636
795914 TA = 161
54971
MA = 161
47205
Ha = 193
637 n
mi
Hp = 181
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13632557
42 X = -4112791
16
Y = -5134628
01 feet Y = -1611262
78 meter
Z = -16616185
85 Z = -5084696
64
XDOT = 14120
698336 XDOT = 4380
421657
YDOT = -20186
280840 feet/sec YDOT = -6104
221126 meter/sec
ZDOT = -5370
065334 ZDOT = -1615
702171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6715116
31 X = -2046767
45
Y = 12825552
91 feet Y = 3909228
53 meter
Z = -16694941
29 Z = -5088618
10
XDOT = -17416
032403 XDOT = -5308
406677
YDOT = -15972
050624 feet/sec YDOT = -4868
281030 meter/sec
ZDOT = -5287
680347 ZDOT = -1611
684970
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
51865767
00010596 00000-0 82463-4 0 9052
2 25544 51
6398 315
4646 0008919 116
7425 243
4651 15
73724005 5695
Satellite: ISS
Catalog Number: 25544
Epoch time: 09166
51865767 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 315
4646 deg
Eccentricity:
0008919
Arg of perigee: 116
7425 deg
Mean anomaly: 243
4651 deg
Mean motion: 15
73724005 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 569
Checksum: 337
Coasting Arc #7 (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 = -3216963
34 A = 6732004
73 meter
Y = 5710914
24 meter E =
0022829
Z = 1486102
57 I = 51
40109
XDOT = -4944
500738 Wp = 119
18127
YDOT = -1268
072015 meter/sec RA = 309
81975 deg
ZDOT = -5774
731896 TA = 44
38402
MA = 44
20126
Ha = 193
541 n
mi
Hp = 181
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10554341
65 X = -3287803
92
Y = 18736595
27 feet Y = 5674544
01 meter
Z = 4875664
61 Z = 1470303
08
XDOT = -16222
115281 XDOT = -4901
900674
YDOT = -4160
341255 feet/sec YDOT = -1323
125426 meter/sec
ZDOT = -18945
970788 ZDOT = -5798
649113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17555006
07 X = 5350765
85
Y = 12444811
00 feet Y = 3793178
39 meter
Z = 4814008
37 Z = 1467309
75
XDOT = -4880
572790 XDOT = -1487
598586
YDOT = 14321
217643 feet/sec YDOT = 4365
107137 meter/sec
ZDOT = -19039
735159 ZDOT = -5803
311276
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
53466688
00010596 00000-0 82463-4 0 9065
2 25544 51
6390 310
2476 0008786 120
9723 239
2304 15
73734136 5853
Satellite: ISS
Catalog Number: 25544
Epoch time: 09167
53466688 = yrday
fracday
Element set: 906
Inclination: 51
6390 deg
RA of node: 310
2476 deg
Eccentricity:
0008786
Arg of perigee: 120
9723 deg
Mean anomaly: 239
2304 deg
Mean motion: 15
73734136 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 585
Checksum: 328
Coasting Arc #8 (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 = 4432170
36 A = 6721721
20 meter
Y = 631358
01 meter E =
0014021
Z = 5006058
43 I = 51
35006
XDOT = -3012
129092 Wp = 124
59005
YDOT = 6864
944161 meter/sec RA = 304
69626 deg
ZDOT = 1789
617494 TA = 308
05030
MA = 308
17674
Ha = 193
252 n
mi
Hp = 181
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14541241
33 X = 4400462
22
Y = 2071384
54 feet Y = 680743
19 meter
Z = 16424076
21 Z = 5027513
20
XDOT = -9882
313294 XDOT = -3097
363918
YDOT = 22522
782682 feet/sec YDOT = 6830
783969 meter/sec
ZDOT = 5871
448470 ZDOT = 1774
778272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3295425
62 X = 1004445
73
Y = -14216514
40 feet Y = -4333193
59 meter
Z = 16508164
68 Z = 5031688
59
XDOT = 20559
005326 XDOT = 6266
384823
YDOT = 11559
605354 feet/sec YDOT = 3523
367712 meter/sec
ZDOT = 5813
606984 ZDOT = 1771
987409
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
55065741
00010596 00000-0 82463-4 0 9074
2 25544 51
6400 305
0321 0008657 124
8145 235
3834 15
73794467 6011
Satellite: ISS
Catalog Number: 25544
Epoch time: 09168
55065741 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 305
0321 deg
Eccentricity:
0008657
Arg of perigee: 124
8145 deg
Mean anomaly: 235
3834 deg
Mean motion: 15
73794467 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 601
Checksum: 305
Coasting Arc #9 (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 = 2029864
54 A = 6731638
86 meter
Y = -6212610
35 meter E =
0011823
Z = -1619062
11 I = 51
36823
XDOT = 5140
566325 Wp = 84
68382
YDOT = 198
546235 meter/sec RA = 299
51269 deg
ZDOT = 5719
944745 TA = 257
38886
MA = 257
52110
Ha = 193
368 n
mi
Hp = 181
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6659660
58 X = 2107049
35
Y = -20382579
90 feet Y = -6189479
42 meter
Z = -5311883
57 Z = -1609014
34
XDOT = 16865
375083 XDOT = 5110
177273
YDOT = 651
398410 feet/sec YDOT = 255
860292 meter/sec
ZDOT = 18766
222918 ZDOT = 5744
844157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19879856
94 X = -6059380
40
Y = -8062614
88 feet Y = -2457485
02 meter
Z = -5272786
63 Z = -1607145
37
XDOT = 1203
123907 XDOT = 366
712167
YDOT = -15223
246159 feet/sec YDOT = -4640
045429 meter/sec
ZDOT = 18863
789602 ZDOT = 5749
683071
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
50313390
00010596 00000-0 82463-4 0 9087
2 25544 51
6408 300
1425 0008714 127
5485 232
6471 15
73790997 6168
Satellite: ISS
Catalog Number: 25544
Epoch time: 09169
50313390 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 300
1425 deg
Eccentricity:
0008714
Arg of perigee: 127
5485 deg
Mean anomaly: 232
6471 deg
Mean motion: 15
73790997 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 616
Checksum: 315
Coasting Arc #10 (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 = -4507093
39 A = 6721765
21 meter
Y = 255030
93 meter E =
0019460
Z = -4996237
43 I = 51
32186
XDOT = 1652
387238 Wp = 97
08547
YDOT = -7270
697689 meter/sec RA = 294
38824 deg
ZDOT = -1870
342686 TA = 154
80234
MA = 154
70727
Ha = 193
198 n
mi
Hp = 181
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14787051
80 X = -4485339
06
Y = 836715
64 feet Y = 204752
48 meter
Z = -16391855
10 Z = -5018080
31
XDOT = 5421
217972 XDOT = 1742
652513
YDOT = -23853
995042 feet/sec YDOT = -7251
714704 meter/sec
ZDOT = -6136
294902 ZDOT = -1862
097284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 87334
65 X = 26619
60
Y = 14715183
09 feet Y = 4485187
81 meter
Z = -16477429
01 Z = -5022320
36
XDOT = -22472
293196 XDOT = -6849
554966
YDOT = -6670
539551 feet/sec YDOT = -2033
180455 meter/sec
ZDOT = -6104
303988 ZDOT = -1860
591856
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
51909041
00010596 00000-0 82463-4 0 9095
2 25544 51
6410 294
9267 0008571 131
2953 228
8949 15
73817392 6322
Satellite: ISS
Catalog Number: 25544
Epoch time: 09170
51909041 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 294
9267 deg
Eccentricity:
0008571
Arg of perigee: 131
2953 deg
Mean anomaly: 228
8949 deg
Mean motion: 15
73817392 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 632
Checksum: 327
Coasting Arc #11 (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 = -844677
39 A = 6731466
88 meter
Y = 6456953
13 meter E =
0022449
Z = 1657548
03 I = 51
34373
XDOT = -5116
673048 Wp = 123
17870
YDOT = 807
334547 meter/sec RA = 289
20078 deg
ZDOT = -5708
881408 TA = 38
40735
MA = 38
24774
Ha = 193
142 n
mi
Hp = 181
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2771251
26 X = -924869
51
Y = 21184229
44 feet Y = 6447058
74 meter
Z = 5438149
70 Z = 1653251
06
XDOT = -16786
985067 XDOT = -5097
587476
YDOT = 2648
735391 feet/sec YDOT = 750
224792 meter/sec
ZDOT = -18729
925878 ZDOT = -5733
691984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21077744
19 X = 6424496
43
Y = 3515667
45 feet Y = 1071575
44 meter
Z = 5421592
49 Z = 1652501
39
XDOT = 2340
758226 XDOT = 713
463107
YDOT = 15220
792199 feet/sec YDOT = 4639
297462 meter/sec
ZDOT = -18827
109542 ZDOT = -5738
502988
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
53502979
00010596 00000-0 82463-4 0 9109
2 25544 51
6412 289
7103 0008630 135
1163 225
0699 15
73834682 6486
Satellite: ISS
Catalog Number: 25544
Epoch time: 09171
53502979 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 289
7103 deg
Eccentricity:
0008630
Arg of perigee: 135
1163 deg
Mean anomaly: 225
0699 deg
Mean motion: 15
73834682 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 648
Checksum: 315
Coasting Arc #12 (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 = 4383049
75 A = 6721605
40 meter
Y = -1147740
17 meter E =
0014148
Z = 4958905
07 I = 51
30359
XDOT = -262
880062 Wp = 132
72867
YDOT = 7452
015212 meter/sec RA = 284
07551 deg
ZDOT = 1944
135106 TA = 298
34012
MA = 298
48275
Ha = 192
832 n
mi
Hp = 181
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14380084
47 X = 4371468
58
Y = -3765551
73 feet Y = -1098792
22 meter
Z = 16269373
59 Z = 4980169
69
XDOT = -862
467394 XDOT = -355
634542
YDOT = 24448
868807 feet/sec YDOT = 7448
556476 meter/sec
ZDOT = 6378
396018 ZDOT = 1942
634412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3528595
08 X = -1075515
78
Y = -14345676
04 feet Y = -4372562
06 meter
Z = 16352654
89 Z = 4984289
21
XDOT = 23384
670910 XDOT = 7127
647693
YDOT = 1560
828435 feet/sec YDOT = 475
740507 meter/sec
ZDOT = 6372
839633 ZDOT = 1942
441520
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
55094949
00010596 00000-0 82463-4 0 9116
2 25544 51
6421 284
4945 0008466 138
7689 221
4115 15
73909730 6649
Satellite: ISS
Catalog Number: 25544
Epoch time: 09172
55094949 = yrday
fracday
Element set: 911
Inclination: 51
6421 deg
RA of node: 284
4945 deg
Eccentricity:
0008466
Arg of perigee: 138
7689 deg
Mean anomaly: 221
4115 deg
Mean motion: 15
73909730 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 664
Checksum: 335
Coasting Arc #13 (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 = -374840
27 A = 6731227
49 meter
Y = -6500161
54 meter E =
0009917
Z = -1717421
04 I = 51
32980
XDOT = 4876
877987 Wp = 92
33277
YDOT = -1774
131052 meter/sec RA = 278
88630 deg
ZDOT = 5678
240849 TA = 248
60038
MA = 248
70621
Ha = 192
894 n
mi
Hp = 181
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1229790
90 X = -293783
58
Y = -21325989
32 feet Y = -6503899
61 meter
Z = -5634583
47 Z = -1719046
67
XDOT = 16000
255863 XDOT = 4868
770303
YDOT = -5820
639933 feet/sec YDOT = -1719
641630 meter/sec
ZDOT = 18629
399110 ZDOT = 5701
912611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21325284
07 X = -6499946
58
Y = 1211358
14 feet Y = 369221
96 meter
Z = -5641241
69 Z = -1719450
47
XDOT = -5742
624599 XDOT = -1750
351978
YDOT = -14332
844417 feet/sec YDOT = -4368
650978 meter/sec
ZDOT = 18722
094750 ZDOT = 5706
494480
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
50336108
00010596 00000-0 82463-4 0 9129
2 25544 51
6422 279
6050 0008308 141
0927 219
0836 15
73878595 6793
Satellite: ISS
Catalog Number: 25544
Epoch time: 09173
50336108 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 279
6050 deg
Eccentricity:
0008308
Arg of perigee: 141
0927 deg
Mean anomaly: 219
0836 deg
Mean motion: 15
73878595 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 679
Checksum: 322
Coasting Arc #14 (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 = -4117373
87 A = 6721613
48 meter
Y = 1912519
98 meter E =
0017696
Z = -4970651
52 I = 51
29415
XDOT = -1079
642096 Wp = 101
63121
YDOT = -7359
703248 meter/sec RA = 273
76047 deg
ZDOT = -1946
800225 TA = 149
48789
MA = 149
38482
Ha = 192
728 n
mi
Hp = 181
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13508444
46 X = -4114307
64
Y = 6274671
87 feet Y = 1866495
39 meter
Z = -16307911
82 Z = -4990645
69
XDOT = -3542
132861 XDOT = -987
807274
YDOT = -24146
008030 feet/sec YDOT = -7371
262515 meter/sec
ZDOT = -6387
139847 ZDOT = -1951
823708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6513098
96 X = 1985192
56
Y = 13299237
99 feet Y = 4053607
74 meter
Z = -16386194
73 Z = -4994512
15
XDOT = -23109
830873 XDOT = -7043
876450
YDOT = 3461
019752 feet/sec YDOT = 1054
918820 meter/sec
ZDOT = -6407
163645 ZDOT = -1952
903479
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
51924878
00010596 00000-0 82463-4 0 9139
2 25544 51
6421 274
3892 0008304 145
7451 214
4250 15
73910324 6951
Satellite: ISS
Catalog Number: 25544
Epoch time: 09174
51924878 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 274
3892 deg
Eccentricity:
0008304
Arg of perigee: 145
7451 deg
Mean anomaly: 214
4250 deg
Mean motion: 15
73910324 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 695
Checksum: 310
Coasting Arc #15 (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 = 1513496
29 A = 6731107
81 meter
Y = 6323503
44 meter E =
0021645
Z = 1693187
49 I = 51
32484
XDOT = -4494
082704 Wp = 127
68292
YDOT = 2610
058458 meter/sec RA = 268
57069 deg
ZDOT = -5694
107492 TA = 33
48539
MA = 33
34874
Ha = 192
661 n
mi
Hp = 181
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4965539
03 X = 1434448
23
Y = 20746402
37 feet Y = 6339985
91 meter
Z = 5555077
06 Z = 1700349
26
XDOT = -14744
365828 XDOT = -4495
274229
YDOT = 8563
183917 feet/sec YDOT = 2559
797511 meter/sec
ZDOT = -18681
455027 ZDOT = -5715
941826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20560745
27 X = 6266915
16
Y = -5657696
33 feet Y = -1724465
84 meter
Z = 5583448
44 Z = 1701835
08
XDOT = 8658
255229 XDOT = 2639
036194
YDOT = 12827
025915 feet/sec YDOT = 3909
677499 meter/sec
ZDOT = -18766
923522 ZDOT = -5720
158290
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
53512011
00010596 00000-0 82463-4 0 9145
2 25544 51
6412 269
1735 0008383 148
4780 211
6886 15
73935344 7113
Satellite: ISS
Catalog Number: 25544
Epoch time: 09175
53512011 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 269
1735 deg
Eccentricity:
0008383
Arg of perigee: 148
4780 deg
Mean anomaly: 211
6886 deg
Mean motion: 15
73935344 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 711
Checksum: 308
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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