Date:
October 1st 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12378 5 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 2253)
---------------------------------------
Vector Time (GMT): 2009/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3825516
69 A = 6730758
12 meter
Y = 5536077
32 meter E =
0013040
Z = -88555
14 I = 51
93162
XDOT = -3944
235189 Wp = 83
02695
YDOT = -2640
746698 meter/sec RA = 125
23563 deg
ZDOT = 6058
598552 TA = 276
01536
MA = 276
16395
Ha = 191
841 n
mi
Hp = 181
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12550907
78 X = -3886707
56
Y = 18162983
33 feet Y = 5492955
99 meter
Z = -290535
23 Z = -107288
64
XDOT = -12940
404162 XDOT = -3943
844455
YDOT = -8663
867121 feet/sec YDOT = -2684
850802 meter/sec
ZDOT = 19877
291836 ZDOT = 6039
438537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9692013
36 X = 2954125
67
Y = -19835221
41 feet Y = -6045775
49 meter
Z = -364044
90 Z = -110960
89
XDOT = 12758
408662 XDOT = 3888
762960
YDOT = 5907
113494 feet/sec YDOT = 1800
488193 meter/sec
ZDOT = 19801
600033 ZDOT = 6035
527690
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 09273
50021567
00020000 00000-0 20000-3 0 9006
2 25544 51
6390 126
1538 0008310 147
0727 213
0956 15
74493860 22548
Satellite: ISS
Catalog Number: 25544
Epoch time: 09273
50021567 = yrday
fracday
Element set: 900
Inclination: 51
6390 deg
RA of node: 126
1538 deg
Eccentricity:
0008310
Arg of perigee: 147
0727 deg
Mean anomaly: 213
0956 deg
Mean motion: 15
74493860 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2254
Checksum: 276
Coasting Arc #2 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2009/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3516807
43 A = 6718619
28 meter
Y = 2212157
82 meter E =
0020483
Z = -5296398
33 I = 51
90587
XDOT = -3944
202363 Wp = 111
55895
YDOT = 6597
480337 meter/sec RA = 120
11464 deg
ZDOT = 129
680424 TA = 159
71000
MA = 159
62849
Ha = 191
726 n
mi
Hp = 181
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11538082
13 X = 3517538
46
Y = 7257735
63 feet Y = 2251488
42 meter
Z = -17376634
93 Z = -5279311
99
XDOT = -12940
296465 XDOT = -4018
313355
YDOT = 21645
276696 feet/sec YDOT = 6552
959578 meter/sec
ZDOT = 425
460708 ZDOT = 110
338714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12685241
74 X = -3866461
68
Y = -5218020
07 feet Y = -1590452
52 meter
Z = -17309142
55 Z = -5275826
65
XDOT = 8777
090699 XDOT = 2675
257245
YDOT = -22573
201390 feet/sec YDOT = -6880
311784 meter/sec
ZDOT = 349
611978 ZDOT = 106
561731
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 09274
51572418
00020000 00000-0 20000-3 0 9015
2 25544 51
6377 120
9334 0008281 150
9355 209
2271 15
74523994 22703
Satellite: ISS
Catalog Number: 25544
Epoch time: 09274
51572418 = yrday
fracday
Element set: 901
Inclination: 51
6377 deg
RA of node: 120
9334 deg
Eccentricity:
0008281
Arg of perigee: 150
9355 deg
Mean anomaly: 209
2271 deg
Mean motion: 15
74523994 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2270
Checksum: 290
Coasting Arc #3 (Orbit 2285)
---------------------------------------
Vector Time (GMT): 2009/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3058980
10 A = 6730622
94 meter
Y = -5975382
13 meter E =
0019653
Z = -315731
14 I = 51
96045
XDOT = 4106
679146 Wp = 144
74722
YDOT = 2411
900843 meter/sec RA = 115
00038 deg
ZDOT = -6059
873779 TA = 38
67267
MA = 38
53210
Ha = 191
634 n
mi
Hp = 181
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10036023
94 X = 3127104
29
Y = -19604272
10 feet Y = -5940793
95 meter
Z = -1035863
32 Z = -300704
34
XDOT = 13473
356779 XDOT = 4108
841758
YDOT = 7913
060510 feet/sec YDOT = 2457
835612 meter/sec
ZDOT = -19881
475653 ZDOT = -6039
918296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6275029
37 X = -1912628
95
Y = 21113781
96 feet Y = 6435480
74 meter
Z = -976980
77 Z = -297783
74
XDOT = -13270
457642 XDOT = -4044
835489
YDOT = -4827
922288 feet/sec YDOT = -1471
550713 meter/sec
ZDOT = -19802
660270 ZDOT = -6035
850850
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 09275
53121582
00020000 00000-0 20000-3 0 9021
2 25544 51
6378 115
7145 0008243 155
0323 205
1241 15
74535370 22865
Satellite: ISS
Catalog Number: 25544
Epoch time: 09275
53121582 = yrday
fracday
Element set: 902
Inclination: 51
6378 deg
RA of node: 115
7145 deg
Eccentricity:
0008243
Arg of perigee: 155
0323 deg
Mean anomaly: 205
1241 deg
Mean motion: 15
74535370 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2286
Checksum: 268
Coasting Arc #4 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2009/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3662109
90 A = 6718639
25 meter
Y = -1994288
36 meter E =
0008610
Z = 5262755
23 I = 51
93080
XDOT = 3030
702192 Wp = 140
07160
YDOT = -7063
019426 meter/sec RA = 109
87337 deg
ZDOT = -573
510603 TA = 315
31744
MA = 315
38679
Ha = 191
636 n
mi
Hp = 181
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12014796
26 X = -3665103
19
Y = -6542940
81 feet Y = -2035256
42 meter
Z = 17266257
32 Z = 5244957
34
XDOT = 9943
248661 XDOT = 3112
242906
YDOT = -23172
635912 feet/sec YDOT = -7028
672470 meter/sec
ZDOT = -1881
596468 ZDOT = -558
588399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13180436
23 X = 4017396
96
Y = 3982916
00 feet Y = 1213992
80 meter
Z = 17195974
14 Z = 5241332
92
XDOT = -4819
550281 XDOT = -1468
998926
YDOT = 23735
905148 feet/sec YDOT = 7234
703889 meter/sec
ZDOT = -1823
182065 ZDOT = -555
705893
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 09276
54668992
00020000 00000-0 20000-3 0 9035
2 25544 51
6368 110
4940 0008253 159
0699 201
0804 15
74545570 23022
Satellite: ISS
Catalog Number: 25544
Epoch time: 09276
54668992 = yrday
fracday
Element set: 903
Inclination: 51
6368 deg
RA of node: 110
4940 deg
Eccentricity:
0008253
Arg of perigee: 159
0699 deg
Mean anomaly: 201
0804 deg
Mean motion: 15
74545570 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2302
Checksum: 299
Coasting Arc #5 (Orbit 2317)
---------------------------------------
Vector Time (GMT): 2009/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2230054
56 A = 6730295
19 meter
Y = 6309794
42 meter E =
0013011
Z = 701186
74 I = 51
97843
XDOT = -4281
599235 Wp = 88
61372
YDOT = -2191
596267 meter/sec RA = 104
76569 deg
ZDOT = 6009
486481 TA = 278
98747
MA = 279
13471
Ha = 191
343 n
mi
Hp = 181
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7316451
97 X = -2303852
34
Y = 20701425
27 feet Y = 6284444
08 meter
Z = 2300481
42 Z = 690173
04
XDOT = -14047
241586 XDOT = -4285
967845
YDOT = -7190
276467 feet/sec YDOT = -2239
499486 meter/sec
ZDOT = 19716
162997 ZDOT = 5988
675619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2659367
04 X = 810575
07
Y = -21799163
04 feet Y = -6644384
89 meter
Z = 2257421
14 Z = 688061
96
XDOT = 13795
804584 XDOT = 4204
961237
YDOT = 3749
072033 feet/sec YDOT = 1142
717156 meter/sec
ZDOT = 19633
992076 ZDOT = 5984
440785
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 09277
56214552
00020000 00000-0 20000-3 0 9048
2 25544 51
6358 105
2728 0008223 163
1190 197
0248 15
74590669 23188
Satellite: ISS
Catalog Number: 25544
Epoch time: 09277
56214552 = yrday
fracday
Element set: 904
Inclination: 51
6358 deg
RA of node: 105
2728 deg
Eccentricity:
0008223
Arg of perigee: 163
1190 deg
Mean anomaly: 197
0248 deg
Mean motion: 15
74590669 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2318
Checksum: 298
Coasting Arc #6 (Orbit 2332)
---------------------------------------
Vector Time (GMT): 2009/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3826495
03 A = 6718707
62 meter
Y = 1857614
01 meter E =
0019189
Z = -5216263
22 I = 51
94574
XDOT = -2089
940205 Wp = 121
80332
YDOT = 7321
800624 meter/sec RA = 99
63129 deg
ZDOT = 1067
296168 TA = 158
39086
MA = 158
30978
Ha = 191
246 n
mi
Hp = 181
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12554117
55 X = 3830778
79
Y = 6094534
14 feet Y = 1900427
68 meter
Z = -17113724
47 Z = -5197663
37
XDOT = -6856
759204 XDOT = -2176
843382
YDOT = 24021
655589 feet/sec YDOT = 7297
943862 meter/sec
ZDOT = 3501
627848 ZDOT = 1056
931324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13728234
78 X = -4184365
96
Y = -2965267
61 feet Y = -903813
57 meter
Z = -17040291
57 Z = -5193880
87
XDOT = 850
990596 XDOT = 259
381934
YDOT = -23962
851912 feet/sec YDOT = -7303
877263 meter/sec
ZDOT = 3461
168765 ZDOT = 1054
964240
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 09278
51411925
00020000 00000-0 20000-3 0 9058
2 25544 51
6354 100
3781 0008289 166
0933 194
0461 15
74622162 23333
Satellite: ISS
Catalog Number: 25544
Epoch time: 09278
51411925 = yrday
fracday
Element set: 905
Inclination: 51
6354 deg
RA of node: 100
3781 deg
Eccentricity:
0008289
Arg of perigee: 166
0933 deg
Mean anomaly: 194
0461 deg
Mean motion: 15
74622162 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2333
Checksum: 283
Coasting Arc #7 (Orbit 2348)
---------------------------------------
Vector Time (GMT): 2009/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1427289
93 A = 6729663
12 meter
Y = -6462868
43 meter E =
0016937
Z = -1166685
42 I = 51
98762
XDOT = 4482
219714 Wp = 155
02106
YDOT = 2050
975086 meter/sec RA = 94
53408 deg
ZDOT = -5923
907693 TA = 37
70768
MA = 37
58909
Ha = 191
007 n
mi
Hp = 181
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4682709
74 X = 1505120
46
Y = -21203636
58 feet Y = -6446472
52 meter
Z = -3827708
07 Z = -1159562
06
XDOT = 14705
445255 XDOT = 4487
730286
YDOT = 6728
920885 feet/sec YDOT = 2101
128407 meter/sec
ZDOT = -19435
392693 ZDOT = -5902
119197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 758936
60 X = 231323
87
Y = 21706164
85 feet Y = 6616039
05 meter
Z = -3799966
65 Z = -1158229
84
XDOT = -14449
098852 XDOT = -4404
085330
YDOT = -2855
608012 feet/sec YDOT = -870
389322 meter/sec
ZDOT = -19349
379380 ZDOT = -5897
690835
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 09279
52953936
00020000 00000-0 20000-3 0 9064
2 25544 51
6360 95
1581 0008047 169
8710 190
2617 15
74679727 23492
Satellite: ISS
Catalog Number: 25544
Epoch time: 09279
52953936 = yrday
fracday
Element set: 906
Inclination: 51
6360 deg
RA of node: 95
1581 deg
Eccentricity:
0008047
Arg of perigee: 169
8710 deg
Mean anomaly: 190
2617 deg
Mean motion: 15
74679727 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2349
Checksum: 328
Coasting Arc #8 (Orbit 2364)
---------------------------------------
Vector Time (GMT): 2009/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4013547
13 A = 6719080
87 meter
Y = -1709545
24 meter E =
0007272
Z = 5104849
90 I = 51
95240
XDOT = 1162
097272 Wp = 137
50699
YDOT = -7451
931783 meter/sec RA = 89
39198 deg
ZDOT = -1585
830516 TA = 327
61744
MA = 327
66205
Ha = 191
137 n
mi
Hp = 181
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13167805
56 X = -4018931
51
Y = -5608744
23 feet Y = -1754457
06 meter
Z = 16748195
20 Z = 5085338
53
XDOT = 3812
655091 XDOT = 1253
043579
YDOT = -24448
595087 feet/sec YDOT = -7438
428062 meter/sec
ZDOT = -5202
856025 ZDOT = -1579
963780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14281607
58 X = 4353033
99
Y = 1859747
58 feet Y = 566851
06 meter
Z = 16671178
17 Z = 5081375
11
XDOT = 2965
609429 XDOT = 903
917754
YDOT = 23545
099599 feet/sec YDOT = 7176
546358 meter/sec
ZDOT = -5180
104478 ZDOT = -1578
895845
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 09280
54494341
00020000 00000-0 20000-3 0 9079
2 25544 51
6357 89
9374 0008261 173
6022 186
5249 15
74643821 23659
Satellite: ISS
Catalog Number: 25544
Epoch time: 09280
54494341 = yrday
fracday
Element set: 907
Inclination: 51
6357 deg
RA of node: 89
9374 deg
Eccentricity:
0008261
Arg of perigee: 173
6022 deg
Mean anomaly: 186
5249 deg
Mean motion: 15
74643821 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2365
Checksum: 310
Coasting Arc #9 (Orbit 2380)
---------------------------------------
Vector Time (GMT): 2009/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -619015
78 A = 6729023
30 meter
Y = 6501747
18 meter E =
0013105
Z = 1613804
69 I = 51
98573
XDOT = -4725
353879 Wp = 98
34644
YDOT = -1893
529757 meter/sec RA = 84
30194 deg
ZDOT = 5774
696188 TA = 279
37985
MA = 279
52800
Ha = 190
794 n
mi
Hp = 181
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2030891
66 X = -699513
20
Y = 21331191
54 feet Y = 6494374
91 meter
Z = 5294634
80 Z = 1610601
87
XDOT = -15503
129525 XDOT = -4731
882009
YDOT = -6212
367968 feet/sec YDOT = -1946
407917 meter/sec
ZDOT = 18945
853634 ZDOT = 5751
724016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4075894
77 X = -1242332
73
Y = -21039523
31 feet Y = -6412846
71 meter
Z = 5282324
46 Z = 1610052
50
XDOT = 15200
125644 XDOT = 4632
998296
YDOT = 1823
507356 feet/sec YDOT = 555
805042 meter/sec
ZDOT = 18855
180205 ZDOT = 5747
058926
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 09281
56032615
00020000 00000-0 20000-3 0 9085
2 25544 51
6364 84
7167 0008274 177
6415 182
4789 15
74714722 23815
Satellite: ISS
Catalog Number: 25544
Epoch time: 09281
56032615 = yrday
fracday
Element set: 908
Inclination: 51
6364 deg
RA of node: 84
7167 deg
Eccentricity:
0008274
Arg of perigee: 177
6415 deg
Mean anomaly: 182
4789 deg
Mean motion: 15
74714722 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2381
Checksum: 312
Coasting Arc #10 (Orbit 2395)
---------------------------------------
Vector Time (GMT): 2009/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4258476
91 A = 6719533
03 meter
Y = 1607120
38 meter E =
0016820
Z = -4957252
85 I = 51
95066
XDOT = -289
101568 Wp = 133
89472
YDOT = 7381
275855 meter/sec RA = 79
15198 deg
ZDOT = 2137
704393 TA = 156
81446
MA = 156
73848
Ha = 190
671 n
mi
Hp = 182
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13971380
93 X = 4264271
22
Y = 5272704
67 feet Y = 1654773
62 meter
Z = -16263952
92 Z = -4936550
67
XDOT = -948
495959 XDOT = -382
003574
YDOT = 24216
784301 feet/sec YDOT = 7377
523492 meter/sec
ZDOT = 7013
465857 ZDOT = 2136
074305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15000058
04 X = -4572017
69
Y = -806464
31 feet Y = -245810
32 meter
Z = -16182241
44 Z = -4932347
19
XDOT = -6385
180369 XDOT = -1946
202976
YDOT = -22303
069981 feet/sec YDOT = -6797
975730 meter/sec
ZDOT = 7007
387182 ZDOT = 2135
851613
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 09282
51223161
00020000 00000-0 20000-3 0 9090
2 25544 51
6374 79
8229 0008243 180
5736 179
5419 15
74733792 23966
Satellite: ISS
Catalog Number: 25544
Epoch time: 09282
51223161 = yrday
fracday
Element set: 909
Inclination: 51
6374 deg
RA of node: 79
8229 deg
Eccentricity:
0008243
Arg of perigee: 180
5736 deg
Mean anomaly: 179
5419 deg
Mean motion: 15
74733792 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2396
Checksum: 318
Coasting Arc #11 (Orbit 2411)
---------------------------------------
Vector Time (GMT): 2009/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -92153
81 A = 6727980
61 meter
Y = -6375820
66 meter E =
0013284
Z = -2124399
13 I = 51
97292
XDOT = 5029
197743 Wp = 164
34997
YDOT = 1773
514931 meter/sec RA = 74
06935 deg
ZDOT = -5561
387274 TA = 39
30704
MA = 39
21069
Ha = 190
424 n
mi
Hp = 182
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -302341
90 X = -10531
33
Y = -20918046
78 feet Y = -6376394
79 meter
Z = -6969813
41 Z = -2124648
61
XDOT = 16499
992595 XDOT = 5036
008818
YDOT = 5818
618540 feet/sec YDOT = 1829
792510 meter/sec
ZDOT = -18246
021239 ZDOT = -5536
938514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6870326
92 X = 2094075
65
Y = 19759475
91 feet Y = 6022688
26 meter
Z = -6971091
06 Z = -2124788
55
XDOT = -16153
135970 XDOT = -4923
475844
YDOT = -762
979050 feet/sec YDOT = -232
556015 meter/sec
ZDOT = -18149
523460 ZDOT = -5531
974751
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 09283
52757760
00020000 00000-0 20000-3 0 9101
2 25544 51
6375 74
6022 0008048 184
6908 175
4182 15
74783968 24121
Satellite: ISS
Catalog Number: 25544
Epoch time: 09283
52757760 = yrday
fracday
Element set: 910
Inclination: 51
6375 deg
RA of node: 74
6022 deg
Eccentricity:
0008048
Arg of perigee: 184
6908 deg
Mean anomaly: 175
4182 deg
Mean motion: 15
74783968 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2412
Checksum: 314
Coasting Arc #12 (Orbit 2427)
---------------------------------------
Vector Time (GMT): 2009/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4535425
88 A = 6720354
51 meter
Y = -1463803
01 meter E =
0007220
Z = 4731428
86 I = 51
93750
XDOT = -501
902182 Wp = 127
78089
YDOT = -7197
482029 meter/sec RA = 68
91030 deg
ZDOT = -2709
399989 TA = 348
73102
MA = 348
74718
Ha = 190
502 n
mi
Hp = 182
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14880006
17 X = -4541704
96
Y = -4802503
33 feet Y = -1514555
90 meter
Z = 15523060
56 Z = 4709380
29
XDOT = -1646
660701 XDOT = -408
219477
YDOT = -23613
786184 feet/sec YDOT = -7202
570801 meter/sec
ZDOT = -8889
107576 ZDOT = -2711
610661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15715161
78 X = 4789981
31
Y = -454347
52 feet Y = -138485
13 meter
Z = 15436038
65 Z = 4704904
58
XDOT = 9330
418119 XDOT = 2843
911443
YDOT = 20590
762855 feet/sec YDOT = 6276
064518 meter/sec
ZDOT = -8898
151813 ZDOT = -2712
156672
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 09284
54290613
00020000 00000-0 20000-3 0 9114
2 25544 51
6375 69
3817 0008154 188
0524 172
0510 15
74761685 24281
Satellite: ISS
Catalog Number: 25544
Epoch time: 09284
54290613 = yrday
fracday
Element set: 911
Inclination: 51
6375 deg
RA of node: 69
3817 deg
Eccentricity:
0008154
Arg of perigee: 188
0524 deg
Mean anomaly: 172
0510 deg
Mean motion: 15
74761685 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2428
Checksum: 297
Coasting Arc #13 (Orbit 2443)
---------------------------------------
Vector Time (GMT): 2009/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 746463
96 A = 6726769
61 meter
Y = 6153231
44 meter E =
0012640
Z = 2610865
90 I = 51
94939
XDOT = -5380
244938 Wp = 112
90787
YDOT = -1594
428102 meter/sec RA = 63
83298 deg
ZDOT = 5271
064280 TA = 276
62732
MA = 276
77118
Ha = 190
069 n
mi
Hp = 182
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2449028
75 X = 664918
77
Y = 20187767
18 feet Y = 6161122
97 meter
Z = 8565833
02 Z = 2614294
00
XDOT = -17651
722239 XDOT = -5387
621968
YDOT = -5231
063328 feet/sec YDOT = -1654
634266 meter/sec
ZDOT = 17293
517978 ZDOT = 5244
908977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9294000
35 X = -2832811
31
Y = -18081169
98 feet Y = -5511140
61 meter
Z = 8579628
82 Z = 2615070
86
XDOT = 17143
152900 XDOT = 5225
233004
YDOT = -616
247727 feet/sec YDOT = -187
832307 meter/sec
ZDOT = 17190
290611 ZDOT = 5239
600578
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 09285
55821098
00020000 00000-0 20000-3 0 9124
2 25544 51
6387 64
1611 0008169 192
8838 167
2118 15
74858146 24443
Satellite: ISS
Catalog Number: 25544
Epoch time: 09285
55821098 = yrday
fracday
Element set: 912
Inclination: 51
6387 deg
RA of node: 64
1611 deg
Eccentricity:
0008169
Arg of perigee: 192
8838 deg
Mean anomaly: 167
2118 deg
Mean motion: 15
74858146 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2444
Checksum: 319
Coasting Arc #14 (Orbit 2458)
---------------------------------------
Vector Time (GMT): 2009/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4877773
57 A = 6721290
01 meter
Y = 1312797
98 meter E =
0012740
Z = -4445553
43 I = 51
91668
XDOT = 1157
598035 Wp = 149
11732
YDOT = 6856
747237 meter/sec RA = 58
66610 deg
ZDOT = 3288
429932 TA = 153
81194
MA = 153
74746
Ha = 189
900 n
mi
Hp = 182
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16003194
14 X = 4884326
98
Y = 4307079
98 feet Y = 1367380
51 meter
Z = -14585149
04 Z = -4421841
17
XDOT = 3797
893815 XDOT = 1064
863937
YDOT = 22495
889884 feet/sec YDOT = 6869
173859 meter/sec
ZDOT = 10788
812112 ZDOT = 3293
827953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16549925
41 X = -5044417
26
Y = 1863903
39 feet Y = 568117
75 meter
Z = -14491568
80 Z = -4417030
17
XDOT = -11554
052417 XDOT = -3521
675177
YDOT = -18372
926183 feet/sec YDOT = -5600
067901 meter/sec
ZDOT = 10810
406522 ZDOT = 3295
011908
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 09286
51004429
00020000 00000-0 20000-3 0 9133
2 25544 51
6390 59
2672 0007978 196
7115 163
3787 15
74848492 24595
Satellite: ISS
Catalog Number: 25544
Epoch time: 09286
51004429 = yrday
fracday
Element set: 913
Inclination: 51
6390 deg
RA of node: 59
2672 deg
Eccentricity:
0007978
Arg of perigee: 196
7115 deg
Mean anomaly: 163
3787 deg
Mean motion: 15
74848492 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2459
Checksum: 330
Coasting Arc #15 (Orbit 2474)
---------------------------------------
Vector Time (GMT): 2009/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 730797
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1238182
07 A = 6725369
51 meter
Y = -5816116
81 meter E =
0008540
Z = -3133418
11 I = 51
91458
XDOT = 5788
175595 Wp = 168
57909
YDOT = 1395
221547 meter/sec RA = 53
59113 deg
ZDOT = -4887
408373 TA = 47
73981
MA = 47
66741
Ha = 189
697 n
mi
Hp = 182
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4062277
14 X = -1157831
48
Y = -19081748
06 feet Y = -5829513
87 meter
Z = -10280243
14 Z = -3139237
64
XDOT = 18990
077412 XDOT = 5795
886198
YDOT = 4577
498514 feet/sec YDOT = 1459
991074 meter/sec
ZDOT = -16034
804373 ZDOT = -4859
270494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10971280
76 X = 3344046
37
Y = 16117335
37 feet Y = 4912563
82 meter
Z = -10303451
01 Z = -3140491
87
XDOT = -18212
476591 XDOT = -5551
162865
YDOT = 2239
606792 feet/sec YDOT = 682
632150 meter/sec
ZDOT = -15923
767367 ZDOT = -4853
564294
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 09287
52531237
00020000 00000-0 20000-3 0 9148
2 25544 51
6393 54
0456 0007938 200
6868 159
3975 15
74882266 24756
Satellite: ISS
Catalog Number: 25544
Epoch time: 09287
52531237 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 54
0456 deg
Eccentricity:
0007938
Arg of perigee: 200
6868 deg
Mean anomaly: 159
3975 deg
Mean motion: 15
74882266 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2475
Checksum: 326
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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