Date:
July 15th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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 1009)
---------------------------------------
Vector Time (GMT): 2009/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1083731
96 A = 6719244
83 meter
Y = 4041775
52 meter E =
0011213
Z = -5265632
56 I = 51
66783
XDOT = -7531
196620 Wp = 114
84032
YDOT = 1530
204177 meter/sec RA = 170
75967 deg
ZDOT = -380
715399 TA = 151
57389
MA = 151
51268
Ha = 189
619 n
mi
Hp = 184
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3555551
06 X = 1064034
91
Y = 13260418
39 feet Y = 4053784
82 meter
Z = -17275697
37 Z = -5260415
28
XDOT = -24708
650328 XDOT = -7545
898454
YDOT = 5020
354911 feet/sec YDOT = 1445
903761 meter/sec
ZDOT = -1249
066269 ZDOT = -417
337270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11106685
02 X = 3385317
60
Y = -8114068
74 feet Y = -2473168
15 meter
Z = -17254964
35 Z = -5259313
13
XDOT = 12849
231736 XDOT = 3916
445833
YDOT = 20513
394124 feet/sec YDOT = 6252
482529 meter/sec
ZDOT = -1392
778884 ZDOT = -424
519004
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 09194
51659774
00010596 00000-0 82463-4 0 9007
2 25544 51
6362 171
6940 0007249 220
8002 139
2619 15
74320561 10106
Satellite: ISS
Catalog Number: 25544
Epoch time: 09194
51659774 = yrday
fracday
Element set: 900
Inclination: 51
6362 deg
RA of node: 171
6940 deg
Eccentricity:
0007249
Arg of perigee: 220
8002 deg
Mean anomaly: 139
2619 deg
Mean motion: 15
74320561 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1010
Checksum: 293
Coasting Arc #2 (Orbit 1025)
---------------------------------------
Vector Time (GMT): 2009/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6467813
37 A = 6731138
41 meter
Y = -1819749
74 meter E =
0014239
Z = 198465
16 I = 51
73791
XDOT = 1467
586747 Wp = 163
16229
YDOT = 4546
476326 meter/sec RA = 165
62069 deg
ZDOT = -6046
199472 TA = 14
68271
MA = 14
64140
Ha = 189
349 n
mi
Hp = 184
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21219860
14 X = 6486717
31
Y = -5970307
56 feet Y = -1747317
19 meter
Z = 651132
42 Z = 229931
45
XDOT = 4814
917148 XDOT = 1446
009460
YDOT = 14916
260913 feet/sec YDOT = 4562
767700 meter/sec
ZDOT = -19836
612440 ZDOT = -6039
121911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13398327
51 X = -4083810
22
Y = -17499595
33 feet Y = -5333876
66 meter
Z = 774592
38 Z = 236095
76
XDOT = 10756
002381 XDOT = 3278
429526
YDOT = -9123
464176 feet/sec YDOT = -2780
831881 meter/sec
ZDOT = -19808
543285 ZDOT = -6037
643993
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 09195
53220718
00010596 00000-0 82463-4 0 9013
2 25544 51
6366 166
4755 0007192 225
8436 134
2136 15
74357923 10267
Satellite: ISS
Catalog Number: 25544
Epoch time: 09195
53220718 = yrday
fracday
Element set: 901
Inclination: 51
6366 deg
RA of node: 166
4755 deg
Eccentricity:
0007192
Arg of perigee: 225
8436 deg
Mean anomaly: 134
2136 deg
Mean motion: 15
74357923 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1026
Checksum: 310
Coasting Arc #3 (Orbit 1041)
---------------------------------------
Vector Time (GMT): 2009/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1470467
56 A = 6719062
62 meter
Y = -3895555
93 meter E =
0005823
Z = 5276120
04 I = 51
72578
XDOT = 7237
761165 Wp = 213
12735
YDOT = -2625
791445 meter/sec RA = 160
49255 deg
ZDOT = 73
717654 TA = 236
14617
MA = 236
20160
Ha = 189
216 n
mi
Hp = 185
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4824368
64 X = -1452427
95
Y = -12780695
30 feet Y = -3911899
28 meter
Z = 17310105
12 Z = 5269019
89
XDOT = 23745
935580 XDOT = 7266
227177
YDOT = -8614
801328 feet/sec YDOT = -2544
695408 meter/sec
ZDOT = 241
855820 ZDOT = 108
947566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9888597
40 X = -3014044
49
Y = 9476760
95 feet Y = 2888516
74 meter
Z = 17281987
38 Z = 5267549
75
XDOT = -16421
859259 XDOT = -5005
382702
YDOT = -17857
028987 feet/sec YDOT = -5442
822435 meter/sec
ZDOT = 380
060091 ZDOT = 115
842316
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 09196
54780467
00010596 00000-0 82463-4 0 9028
2 25544 51
6365 161
2573 0007232 230
0953 129
9575 15
74364502 10421
Satellite: ISS
Catalog Number: 25544
Epoch time: 09196
54780467 = yrday
fracday
Element set: 902
Inclination: 51
6365 deg
RA of node: 161
2573 deg
Eccentricity:
0007232
Arg of perigee: 230
0953 deg
Mean anomaly: 129
9575 deg
Mean motion: 15
74364502 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1042
Checksum: 309
Coasting Arc #4 (Orbit 1057)
---------------------------------------
Vector Time (GMT): 2009/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6141689
45 A = 6731015
31 meter
Y = 2746039
26 meter E =
0005232
Z = 81692
99 I = 51
79396
XDOT = -1874
515815 Wp = 35
93376
YDOT = -4378
085269 meter/sec RA = 155
36226 deg
ZDOT = 6048
787009 TA = 324
95161
MA = 324
98603
Ha = 188
970 n
mi
Hp = 185
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20149899
77 X = -6172336
51
Y = 9009315
14 feet Y = 2677187
92 meter
Z = 268021
61 Z = 51782
52
XDOT = -6149
986269 XDOT = -1854
803969
YDOT = -14363
796814 feet/sec YDOT = -4398
937782 meter/sec
ZDOT = 19845
101735 ZDOT = 6039
727897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16347413
12 X = 4982691
52
Y = 14832310
30 feet Y = 4520888
18 meter
Z = 150702
04 Z = 45933
98
XDOT = -9553
552585 XDOT = -2911
922828
YDOT = 10316
877302 feet/sec YDOT = 3144
584202 meter/sec
ZDOT = 19809
262856 ZDOT = 6037
863318
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 09197
56338798
00010596 00000-0 82463-4 0 9038
2 25544 51
6362 156
0383 0007265 233
2978 126
7518 15
74407449 10584
Satellite: ISS
Catalog Number: 25544
Epoch time: 09197
56338798 = yrday
fracday
Element set: 903
Inclination: 51
6362 deg
RA of node: 156
0383 deg
Eccentricity:
0007265
Arg of perigee: 233
2978 deg
Mean anomaly: 126
7518 deg
Mean motion: 15
74407449 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1058
Checksum: 342
Coasting Arc #5 (Orbit 1072)
---------------------------------------
Vector Time (GMT): 2009/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1796655
89 A = 6718968
34 meter
Y = 3760450
73 meter E =
0009836
Z = -5277968
51 I = 51
78059
XDOT = -6780
092202 Wp = 116
26590
YDOT = 3629
478964 meter/sec RA = 150
23107 deg
ZDOT = 274
073194 TA = 156
35499
MA = 156
30975
Ha = 188
748 n
mi
Hp = 185
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5894540
34 X = 1780111
81
Y = 12337436
78 feet Y = 3780450
30 meter
Z = -17316169
64 Z = -5269279
94
XDOT = -22244
396989 XDOT = -6821
505141
YDOT = 11907
739384 feet/sec YDOT = 3553
428411 meter/sec
ZDOT = 899
190270 ZDOT = 241
035426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8707148
63 X = 2653938
90
Y = -10598671
02 feet Y = -3230474
93 meter
Z = -17281823
34 Z = -5267499
76
XDOT = 19336
996938 XDOT = 5893
916667
YDOT = 14610
294864 feet/sec YDOT = 4453
217875 meter/sec
ZDOT = 769
620315 ZDOT = 234
580272
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 09198
51548710
00010596 00000-0 82463-4 0 9042
2 25544 51
6369 151
1454 0007258 238
3409 121
7047 15
74403278 10738
Satellite: ISS
Catalog Number: 25544
Epoch time: 09198
51548710 = yrday
fracday
Element set: 904
Inclination: 51
6369 deg
RA of node: 151
1454 deg
Eccentricity:
0007258
Arg of perigee: 238
3409 deg
Mean anomaly: 121
7047 deg
Mean motion: 15
74403278 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1073
Checksum: 310
Coasting Arc #6 (Orbit 1088)
---------------------------------------
Vector Time (GMT): 2009/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5678248
33 A = 6730911
57 meter
Y = -3577256
22 meter E =
0011951
Z = -399203
82 I = 51
84704
XDOT = 2238
794932 Wp = 174
20381
YDOT = 4224
824955 meter/sec RA = 145
11095 deg
ZDOT = -6041
322154 TA = 10
12676
MA = 10
10270
Ha = 188
545 n
mi
Hp = 185
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18629423
65 X = 5719767
05
Y = -11736404
92 feet Y = -3513526
51 meter
Z = -1309723
83 Z = -371518
72
XDOT = 7345
127729 XDOT = 2220
733421
YDOT = 13860
974263 feet/sec YDOT = 4249
760552 meter/sec
ZDOT = -19820
610741 ZDOT = -6030
489229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18650124
05 X = -5684557
81
Y = -11715122
42 feet Y = -3570769
31 meter
Z = -1201158
57 Z = -366113
13
XDOT = 8407
913508 XDOT = 2562
732037
YDOT = -11367
303789 feet/sec YDOT = -3464
754195 meter/sec
ZDOT = -19777
813754 ZDOT = -6028
277632
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 09199
53104656
00010596 00000-0 82463-4 0 9053
2 25544 51
6376 145
9267 0007264 242
4182 117
6244 15
74425002 10899
Satellite: ISS
Catalog Number: 25544
Epoch time: 09199
53104656 = yrday
fracday
Element set: 905
Inclination: 51
6376 deg
RA of node: 145
9267 deg
Eccentricity:
0007264
Arg of perigee: 242
4182 deg
Mean anomaly: 117
6244 deg
Mean motion: 15
74425002 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1089
Checksum: 312
Coasting Arc #7 (Orbit 1104)
---------------------------------------
Vector Time (GMT): 2009/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2111894
28 A = 6718906
63 meter
Y = -3620218
32 meter E =
0004408
Z = 5254784
76 I = 51
83122
XDOT = 6187
107850 Wp = 248
03759
YDOT = -4537
333884 meter/sec RA = 139
97786 deg
ZDOT = -641
386411 TA = 208
03298
MA = 208
05672
Ha = 188
301 n
mi
Hp = 185
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6928787
01 X = -2096782
03
Y = -11877356
69 feet Y = -3643751
26 meter
Z = 17240107
48 Z = 5244561
27
XDOT = 20298
910269 XDOT = 6240
500967
YDOT = -14886
266025 feet/sec YDOT = -4467
847365 meter/sec
ZDOT = -2104
286124 ZDOT = -611
200826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7462520
43 X = -2274576
23
Y = 11609515
65 feet Y = 3538580
37 meter
Z = 17199736
40 Z = 5242479
66
XDOT = -21568
434220 XDOT = -6574
058750
YDOT = -10931
797116 feet/sec YDOT = -3332
011761 meter/sec
ZDOT = -1985
929547 ZDOT = -605
311326
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 09200
54659252
00010596 00000-0 82463-4 0 9065
2 25544 51
6381 140
7084 0007289 246
8660 113
1736 15
74459885 11053
Satellite: ISS
Catalog Number: 25544
Epoch time: 09200
54659252 = yrday
fracday
Element set: 906
Inclination: 51
6381 deg
RA of node: 140
7084 deg
Eccentricity:
0007289
Arg of perigee: 246
8660 deg
Mean anomaly: 113
1736 deg
Mean motion: 15
74459885 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1105
Checksum: 318
Coasting Arc #8 (Orbit 1120)
---------------------------------------
Vector Time (GMT): 2009/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5105995
14 A = 6730625
51 meter
Y = 4317387
34 meter E =
0006863
Z = 730814
69 I = 51
89300
XDOT = -2584
049940 Wp = 33
23660
YDOT = -4075
338190 meter/sec RA = 134
86631 deg
ZDOT = 6000
815486 TA = 334
70003
MA = 334
73363
Ha = 188
002 n
mi
Hp = 185
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16751952
57 X = -5157443
53
Y = 14164656
62 feet Y = 4260001
31 meter
Z = 2397686
01 Z = 705885
97
XDOT = -8477
854134 XDOT = -2567
437221
YDOT = -13370
532121 feet/sec YDOT = -4104
142796 meter/sec
ZDOT = 19687
714849 ZDOT = 5988
301928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20325395
97 X = 6195180
69
Y = 8282680
27 feet Y = 2524560
95 meter
Z = 2299955
76 Z = 701026
52
XDOT = -7255
398904 XDOT = -2211
445586
YDOT = 12331
536302 feet/sec YDOT = 3758
652265 meter/sec
ZDOT = 19638
314948 ZDOT = 5985
758396
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 09201
56212604
00010596 00000-0 82463-4 0 9075
2 25544 51
6383 135
4888 0007296 250
8504 109
1869 15
74470314 11218
Satellite: ISS
Catalog Number: 25544
Epoch time: 09201
56212604 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 135
4888 deg
Eccentricity:
0007296
Arg of perigee: 250
8504 deg
Mean anomaly: 109
1869 deg
Mean motion: 15
74470314 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1121
Checksum: 303
Coasting Arc #9 (Orbit 1135)
---------------------------------------
Vector Time (GMT): 2009/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2404562
08 A = 6719041
55 meter
Y = 3504729
93 meter E =
0008318
Z = -5210742
88 I = 51
87538
XDOT = -5474
315739 Wp = 118
11483
YDOT = 5308
241537 meter/sec RA = 129
72881 deg
ZDOT = 1041
534667 TA = 161
80604
MA = 161
77626
Ha = 187
750 n
mi
Hp = 185
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7888983
20 X = 2390505
20
Y = 11498457
78 feet Y = 3531541
44 meter
Z = -17095613
11 Z = -5199095
30
XDOT = -17960
353475 XDOT = -5538
326022
YDOT = 17415
490607 feet/sec YDOT = 5246
666457 meter/sec
ZDOT = 3417
108488 ZDOT = 1014
786408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6266621
95 X = 1910066
37
Y = -12519973
97 feet Y = -3816088
07 meter
Z = -17049641
52 Z = -5196730
74
XDOT = 22987
183053 XDOT = 7006
493395
YDOT = 6983
579838 feet/sec YDOT = 2128
595135 meter/sec
ZDOT = 3312
266487 ZDOT = 1009
578825
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 09202
51417667
00010596 00000-0 82463-4 0 9088
2 25544 51
6393 130
5961 0007295 254
8012 105
2345 15
74489356 11362
Satellite: ISS
Catalog Number: 25544
Epoch time: 09202
51417667 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 130
5961 deg
Eccentricity:
0007295
Arg of perigee: 254
8012 deg
Mean anomaly: 105
2345 deg
Mean motion: 15
74489356 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1136
Checksum: 310
Coasting Arc #10 (Orbit 1151)
---------------------------------------
Vector Time (GMT): 2009/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4443104
52 A = 6730258
07 meter
Y = -4927174
08 meter E =
0009179
Z = -1093267
90 I = 51
93222
XDOT = 2920
315189 Wp = 187
96654
YDOT = 3949
335637 meter/sec RA = 124
62767 deg
ZDOT = -5933
652723 TA = 3
95197
MA = 3
94472
Ha = 187
543 n
mi
Hp = 185
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14577114
57 X = 4503181
57
Y = -16165269
28 feet Y = -4877152
62 meter
Z = -3586836
95 Z = -1071538
58
XDOT = 9581
086578 XDOT = 2904
759909
YDOT = 12957
137916 feet/sec YDOT = 3981
906163 meter/sec
ZDOT = -19467
364578 ZDOT = -5919
503408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21266663
90 X = -6482079
16
Y = -4705397
19 feet Y = -1434205
06 meter
Z = -3501691
48 Z = -1067315
56
XDOT = 6132
627116 XDOT = 1869
224745
YDOT = -13278
915701 feet/sec YDOT = -4047
413506 meter/sec
ZDOT = -19411
528208 ZDOT = -5916
633798
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 09203
52968505
00010596 00000-0 82463-4 0 9093
2 25544 51
6401 125
3775 0007321 258
3795 101
6547 15
74500187 11522
Satellite: ISS
Catalog Number: 25544
Epoch time: 09203
52968505 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 125
3775 deg
Eccentricity:
0007321
Arg of perigee: 258
3795 deg
Mean anomaly: 101
6547 deg
Mean motion: 15
74500187 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1152
Checksum: 305
Coasting Arc #11 (Orbit 1167)
---------------------------------------
Vector Time (GMT): 2009/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2703618
76 A = 6719196
76 meter
Y = -3393680
61 meter E =
0004024
Z = 5133861
84 I = 51
91117
XDOT = 4675
606173 Wp = 295
94430
YDOT = -5939
234799 meter/sec RA = 119
48617 deg
ZDOT = -1462
931567 TA = 168
03105
MA = 168
02148
Ha = 187
098 n
mi
Hp = 185
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8870140
30 X = -2690407
87
Y = -11134122
74 feet Y = -3423840
73 meter
Z = 16843378
74 Z = 5120759
71
XDOT = 15339
915266 XDOT = 4748
778694
YDOT = -19485
678474 feet/sec YDOT = -5886
540149 meter/sec
ZDOT = -4799
644249 ZDOT = -1440
040918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5020056
25 X = -1530113
15
Y = 13386032
79 feet Y = 4080062
80 meter
Z = 16791683
85 Z = 5118105
24
XDOT = -23618
383366 XDOT = -7198
883250
YDOT = -2945
649881 feet/sec YDOT = -897
834084 meter/sec
ZDOT = -4709
982548 ZDOT = -1435
602681
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 09204
54517920
00010596 00000-0 82463-4 0 9109
2 25544 51
6398 120
1588 0007388 263
1506 96
8817 15
74555244 11685
Satellite: ISS
Catalog Number: 25544
Epoch time: 09204
54517920 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 120
1588 deg
Eccentricity:
0007388
Arg of perigee: 263
1506 deg
Mean anomaly: 96
8817 deg
Mean motion: 15
74555244 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1168
Checksum: 324
Coasting Arc #12 (Orbit 1183)
---------------------------------------
Vector Time (GMT): 2009/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3714805
03 A = 6729727
88 meter
Y = 5409654
28 meter E =
0008112
Z = 1468673
97 I = 51
96026
XDOT = -3269
470592 Wp = 38
11637
YDOT = -3830
159711 meter/sec RA = 114
39259 deg
ZDOT = 5827
471940 TA = 337
98307
MA = 338
01789
Ha = 186
696 n
mi
Hp = 185
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12187680
55 X = -3782155
02
Y = 17748209
58 feet Y = 5367736
46 meter
Z = 4818484
17 Z = 1450464
67
XDOT = -10726
609555 XDOT = -3254
706301
YDOT = -12566
140784 feet/sec YDOT = -3866
638753 meter/sec
ZDOT = 19119
002428 ZDOT = 5811
624749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21517025
99 X = 6558389
52
Y = 1112675
00 feet Y = 339143
34 meter
Z = 4747192
53 Z = 1446944
28
XDOT = -4948
789335 XDOT = -1508
390989
YDOT = 14244
062163 feet/sec YDOT = 4341
590147 meter/sec
ZDOT = 19056
488044 ZDOT = 5808
417556
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 09205
56066227
00010596 00000-0 82463-4 0 9112
2 25544 51
6400 114
9390 0007321 267
2590 92
7735 15
74541213 11849
Satellite: ISS
Catalog Number: 25544
Epoch time: 09205
56066227 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 114
9390 deg
Eccentricity:
0007321
Arg of perigee: 267
2590 deg
Mean anomaly: 92
7735 deg
Mean motion: 15
74541213 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1184
Checksum: 291
Coasting Arc #13 (Orbit 1198)
---------------------------------------
Vector Time (GMT): 2009/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3017429
86 A = 6719627
66 meter
Y = 3294423
02 meter E =
0006250
Z = -5024996
82 I = 51
93822
XDOT = -3817
539532 Wp = 119
94889
YDOT = 6406
157778 meter/sec RA = 109
24533 deg
ZDOT = 1906
254585 TA = 168
39175
MA = 168
37733
Ha = 186
562 n
mi
Hp = 185
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9899704
26 X = 3004776
92
Y = 10808474
48 feet Y = 3328095
27 meter
Z = -16486210
03 Z = -5010368
90
XDOT = -12524
735996 XDOT = -3898
150642
YDOT = 21017
578011 feet/sec YDOT = 6363
016971 meter/sec
ZDOT = 6254
116093 ZDOT = 1887
513891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3729170
95 X = 1136651
30
Y = -14241470
02 feet Y = -4340800
06 meter
Z = -16428517
94 Z = -5007412
27
XDOT = 23435
810379 XDOT = 7143
235003
YDOT = -998
147564 feet/sec YDOT = -304
235378 meter/sec
ZDOT = 6180
784557 ZDOT = 1883
903133
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 09206
51266391
00010596 00000-0 82463-4 0 9123
2 25544 51
6404 110
0458 0007384 270
8654 89
1664 15
74577012 11998
Satellite: ISS
Catalog Number: 25544
Epoch time: 09206
51266391 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 110
0458 deg
Eccentricity:
0007384
Arg of perigee: 270
8654 deg
Mean anomaly: 89
1664 deg
Mean motion: 15
74577012 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1199
Checksum: 311
Coasting Arc #14 (Orbit 1214)
---------------------------------------
Vector Time (GMT): 2009/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2954936
65 A = 6729073
18 meter
Y = -5745490
17 meter E =
0005957
Z = -1866795
59 I = 51
97870
XDOT = 3640
190786 Wp = 210
14817
YDOT = 3717
726079 meter/sec RA = 104
16013 deg
ZDOT = -5677
390591 TA = 350
48377
MA = 350
49505
Ha = 186
670 n
mi
Hp = 185
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9694674
05 X = 3028032
54
Y = -18850033
37 feet Y = -5712037
52 meter
Z = -6124657
43 Z = -1852263
48
XDOT = 11942
883156 XDOT = 3625
927408
YDOT = 12197
264040 feet/sec YDOT = 3758
353429 meter/sec
ZDOT = -18626
609549 ZDOT = -5659
741161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21087311
19 X = -6427412
45
Y = 2308385
27 feet Y = 703595
83 meter
Z = -6067829
59 Z = -1849474
46
XDOT = 3673
345722 XDOT = 1119
635776
YDOT = -15246
457602 feet/sec YDOT = -4647
120277 meter/sec
ZDOT = -18557
015948 ZDOT = -5656
178461
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 09207
52812058
00010596 00000-0 82463-4 0 9133
2 25544 51
6405 104
8262 0007497 273
9771 86
0535 15
74567188 12157
Satellite: ISS
Catalog Number: 25544
Epoch time: 09207
52812058 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 104
8262 deg
Eccentricity:
0007497
Arg of perigee: 273
9771 deg
Mean anomaly: 86
0535 deg
Mean motion: 15
74567188 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1215
Checksum: 320
Coasting Arc #15 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2009/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3354633
04 A = 6720075
80 meter
Y = -3192728
71 meter E =
0005065
Z = 4872681
86 I = 51
95508
XDOT = 2940
078098 Wp = 340
86412
YDOT = -6709
801566 meter/sec RA = 99
00712 deg
ZDOT = -2368
357586 TA = 132
15006
MA = 132
10702
Ha = 187
077 n
mi
Hp = 185
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11006013
93 X = -3342352
51
Y = -10474831
72 feet Y = -3230173
86 meter
Z = 15986489
04 Z = 4856414
78
XDOT = 9645
925519 XDOT = 3026
394696
YDOT = -22013
784666 feet/sec YDOT = -6676
441103 meter/sec
ZDOT = -7770
202055 ZDOT = -2353
865604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2336731
11 X = -712235
64
Y = 15081126
57 feet Y = 4596727
38 meter
Z = 15922361
10 Z = 4853135
66
XDOT = -22528
806463 XDOT = -6866
780210
YDOT = 4667
011202 feet/sec YDOT = 1422
505014 meter/sec
ZDOT = -7713
573338 ZDOT = -2351
097154
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 09208
54356252
00010596 00000-0 82463-4 0 9146
2 25544 51
6403 99
6064 0007571 279
4223 80
6085 15
74650800 12314
Satellite: ISS
Catalog Number: 25544
Epoch time: 09208
54356252 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 99
6064 deg
Eccentricity:
0007571
Arg of perigee: 279
4223 deg
Mean anomaly: 80
6085 deg
Mean motion: 15
74650800 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1231
Checksum: 300
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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